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You searched for subject:( DRNTU Engineering Aeronautical engineering Aerodynamics). Showing records 1 – 30 of 219417 total matches.

[1] [2] [3] [4] [5] … [7314]

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Nanyang Technological University

1. Dominic Denver John Chandar. Computational modeling of unsteady low Reynolds number flapping wing aerodynamics .

Degree: 2010, Nanyang Technological University

 The unsteady low Reynolds number aerodynamics of biomimetic airfoils and wings stands out as one of the most challenging areas of research to the scientific… (more)

Subjects/Keywords: DRNTU::Engineering::Aeronautical engineering::Aerodynamics

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APA (6th Edition):

Chandar, D. D. J. (2010). Computational modeling of unsteady low Reynolds number flapping wing aerodynamics . (Thesis). Nanyang Technological University. Retrieved from http://hdl.handle.net/10356/47219

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Chandar, Dominic Denver John. “Computational modeling of unsteady low Reynolds number flapping wing aerodynamics .” 2010. Thesis, Nanyang Technological University. Accessed January 21, 2020. http://hdl.handle.net/10356/47219.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Chandar, Dominic Denver John. “Computational modeling of unsteady low Reynolds number flapping wing aerodynamics .” 2010. Web. 21 Jan 2020.

Vancouver:

Chandar DDJ. Computational modeling of unsteady low Reynolds number flapping wing aerodynamics . [Internet] [Thesis]. Nanyang Technological University; 2010. [cited 2020 Jan 21]. Available from: http://hdl.handle.net/10356/47219.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Chandar DDJ. Computational modeling of unsteady low Reynolds number flapping wing aerodynamics . [Thesis]. Nanyang Technological University; 2010. Available from: http://hdl.handle.net/10356/47219

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Nanyang Technological University

2. Wanchai, Jiajan. Studies of aerodynamics of supersonic generic round shaped bodies .

Degree: 2014, Nanyang Technological University

 The purpose of this thesis is to study the external flow over the spin-stabilized rounds at supersonic speeds which is beyond the nominal flight of… (more)

Subjects/Keywords: DRNTU::Engineering::Aeronautical engineering::Aerodynamics

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APA (6th Edition):

Wanchai, J. (2014). Studies of aerodynamics of supersonic generic round shaped bodies . (Thesis). Nanyang Technological University. Retrieved from http://hdl.handle.net/10356/58905

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Wanchai, Jiajan. “Studies of aerodynamics of supersonic generic round shaped bodies .” 2014. Thesis, Nanyang Technological University. Accessed January 21, 2020. http://hdl.handle.net/10356/58905.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Wanchai, Jiajan. “Studies of aerodynamics of supersonic generic round shaped bodies .” 2014. Web. 21 Jan 2020.

Vancouver:

Wanchai J. Studies of aerodynamics of supersonic generic round shaped bodies . [Internet] [Thesis]. Nanyang Technological University; 2014. [cited 2020 Jan 21]. Available from: http://hdl.handle.net/10356/58905.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Wanchai J. Studies of aerodynamics of supersonic generic round shaped bodies . [Thesis]. Nanyang Technological University; 2014. Available from: http://hdl.handle.net/10356/58905

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Nanyang Technological University

3. Mao, Rong Hai. Two-stream mixing flow with streamwise vorticity .

Degree: 2005, Nanyang Technological University

 The aerodynamic characteristics of the single-lobe forced mixer have been extensively examined in the present dissertation. Nine single-lobe models with different parameters and geometry configurations… (more)

Subjects/Keywords: DRNTU::Engineering::Aeronautical engineering::Aerodynamics

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APA (6th Edition):

Mao, R. H. (2005). Two-stream mixing flow with streamwise vorticity . (Thesis). Nanyang Technological University. Retrieved from http://hdl.handle.net/10356/6136

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Mao, Rong Hai. “Two-stream mixing flow with streamwise vorticity .” 2005. Thesis, Nanyang Technological University. Accessed January 21, 2020. http://hdl.handle.net/10356/6136.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Mao, Rong Hai. “Two-stream mixing flow with streamwise vorticity .” 2005. Web. 21 Jan 2020.

Vancouver:

Mao RH. Two-stream mixing flow with streamwise vorticity . [Internet] [Thesis]. Nanyang Technological University; 2005. [cited 2020 Jan 21]. Available from: http://hdl.handle.net/10356/6136.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Mao RH. Two-stream mixing flow with streamwise vorticity . [Thesis]. Nanyang Technological University; 2005. Available from: http://hdl.handle.net/10356/6136

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Nanyang Technological University

4. Ang, Jia Liang. Fiber optics flow measuring techniques and feasibility study of its implementation as an angle of attack sensor and stall detector .

Degree: 2014, Nanyang Technological University

 There is a continuous demand to reduce the cost of energy from wind turbine generators. Active control techniques were found to achieve significant savings in… (more)

Subjects/Keywords: DRNTU::Engineering::Mechanical engineering::Fluid mechanics; DRNTU::Engineering::Electrical and electronic engineering::Optics, optoelectronics, photonics; DRNTU::Engineering::Aeronautical engineering::Aerodynamics

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APA (6th Edition):

Ang, J. L. (2014). Fiber optics flow measuring techniques and feasibility study of its implementation as an angle of attack sensor and stall detector . (Thesis). Nanyang Technological University. Retrieved from http://hdl.handle.net/10356/61052

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Ang, Jia Liang. “Fiber optics flow measuring techniques and feasibility study of its implementation as an angle of attack sensor and stall detector .” 2014. Thesis, Nanyang Technological University. Accessed January 21, 2020. http://hdl.handle.net/10356/61052.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Ang, Jia Liang. “Fiber optics flow measuring techniques and feasibility study of its implementation as an angle of attack sensor and stall detector .” 2014. Web. 21 Jan 2020.

Vancouver:

Ang JL. Fiber optics flow measuring techniques and feasibility study of its implementation as an angle of attack sensor and stall detector . [Internet] [Thesis]. Nanyang Technological University; 2014. [cited 2020 Jan 21]. Available from: http://hdl.handle.net/10356/61052.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Ang JL. Fiber optics flow measuring techniques and feasibility study of its implementation as an angle of attack sensor and stall detector . [Thesis]. Nanyang Technological University; 2014. Available from: http://hdl.handle.net/10356/61052

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Nanyang Technological University

5. Chin, Yao Wei. Design and development of energy-efficient mechanism for flapping-wing micro air vehicle .

Degree: 2019, Nanyang Technological University

 Flapping-wing flight provides versatile maneuvers such as vertical takeoff, hover, glide, dash and rapid turn, which can be used for all types of aerial mission.… (more)

Subjects/Keywords: DRNTU::Engineering::Aeronautical engineering

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APA (6th Edition):

Chin, Y. W. (2019). Design and development of energy-efficient mechanism for flapping-wing micro air vehicle . (Thesis). Nanyang Technological University. Retrieved from http://hdl.handle.net/10220/47635

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Chin, Yao Wei. “Design and development of energy-efficient mechanism for flapping-wing micro air vehicle .” 2019. Thesis, Nanyang Technological University. Accessed January 21, 2020. http://hdl.handle.net/10220/47635.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Chin, Yao Wei. “Design and development of energy-efficient mechanism for flapping-wing micro air vehicle .” 2019. Web. 21 Jan 2020.

Vancouver:

Chin YW. Design and development of energy-efficient mechanism for flapping-wing micro air vehicle . [Internet] [Thesis]. Nanyang Technological University; 2019. [cited 2020 Jan 21]. Available from: http://hdl.handle.net/10220/47635.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Chin YW. Design and development of energy-efficient mechanism for flapping-wing micro air vehicle . [Thesis]. Nanyang Technological University; 2019. Available from: http://hdl.handle.net/10220/47635

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Nanyang Technological University

6. Airil Seet Azry Seet. Investigation of flow over oscillating NACA 4421airfoils in tandem configuration at low Reynolds number .

Degree: 2019, Nanyang Technological University

 The present study is on the experimental investigation of the flow over oscillating NACA4421 airfoils in various tandem configurations at low Reynolds number of 8.6… (more)

Subjects/Keywords: DRNTU::Engineering::Aeronautical engineering

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APA (6th Edition):

Seet, A. S. A. (2019). Investigation of flow over oscillating NACA 4421airfoils in tandem configuration at low Reynolds number . (Thesis). Nanyang Technological University. Retrieved from http://hdl.handle.net/10220/47648

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Seet, Airil Seet Azry. “Investigation of flow over oscillating NACA 4421airfoils in tandem configuration at low Reynolds number .” 2019. Thesis, Nanyang Technological University. Accessed January 21, 2020. http://hdl.handle.net/10220/47648.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Seet, Airil Seet Azry. “Investigation of flow over oscillating NACA 4421airfoils in tandem configuration at low Reynolds number .” 2019. Web. 21 Jan 2020.

Vancouver:

Seet ASA. Investigation of flow over oscillating NACA 4421airfoils in tandem configuration at low Reynolds number . [Internet] [Thesis]. Nanyang Technological University; 2019. [cited 2020 Jan 21]. Available from: http://hdl.handle.net/10220/47648.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Seet ASA. Investigation of flow over oscillating NACA 4421airfoils in tandem configuration at low Reynolds number . [Thesis]. Nanyang Technological University; 2019. Available from: http://hdl.handle.net/10220/47648

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Nanyang Technological University

7. Prakash, Rakesh. Optimal algorithms for sequencing of aircraft arrivals and departures .

Degree: 2019, Nanyang Technological University

 In airport operations, runways are scarce and expensive resources and constitute a key bottleneck. Further, capacity on the runway is limited by the safety separation… (more)

Subjects/Keywords: DRNTU::Engineering::Aeronautical engineering

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APA (6th Edition):

Prakash, R. (2019). Optimal algorithms for sequencing of aircraft arrivals and departures . (Thesis). Nanyang Technological University. Retrieved from http://hdl.handle.net/10220/47683

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Prakash, Rakesh. “Optimal algorithms for sequencing of aircraft arrivals and departures .” 2019. Thesis, Nanyang Technological University. Accessed January 21, 2020. http://hdl.handle.net/10220/47683.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Prakash, Rakesh. “Optimal algorithms for sequencing of aircraft arrivals and departures .” 2019. Web. 21 Jan 2020.

Vancouver:

Prakash R. Optimal algorithms for sequencing of aircraft arrivals and departures . [Internet] [Thesis]. Nanyang Technological University; 2019. [cited 2020 Jan 21]. Available from: http://hdl.handle.net/10220/47683.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Prakash R. Optimal algorithms for sequencing of aircraft arrivals and departures . [Thesis]. Nanyang Technological University; 2019. Available from: http://hdl.handle.net/10220/47683

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Nanyang Technological University

8. Low, Chee Meng. Evaluation and mitigation of modelling errors in numerical simulations of mooring line and seabed contact .

Degree: 2019, Nanyang Technological University

 Time-domain mooring simulation is a direct and effective method of evaluating mooring line loads and floater motions, in which nonlinear effects including drag forces and… (more)

Subjects/Keywords: DRNTU::Engineering::Aeronautical engineering

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APA (6th Edition):

Low, C. M. (2019). Evaluation and mitigation of modelling errors in numerical simulations of mooring line and seabed contact . (Thesis). Nanyang Technological University. Retrieved from http://hdl.handle.net/10220/48561

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Low, Chee Meng. “Evaluation and mitigation of modelling errors in numerical simulations of mooring line and seabed contact .” 2019. Thesis, Nanyang Technological University. Accessed January 21, 2020. http://hdl.handle.net/10220/48561.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Low, Chee Meng. “Evaluation and mitigation of modelling errors in numerical simulations of mooring line and seabed contact .” 2019. Web. 21 Jan 2020.

Vancouver:

Low CM. Evaluation and mitigation of modelling errors in numerical simulations of mooring line and seabed contact . [Internet] [Thesis]. Nanyang Technological University; 2019. [cited 2020 Jan 21]. Available from: http://hdl.handle.net/10220/48561.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Low CM. Evaluation and mitigation of modelling errors in numerical simulations of mooring line and seabed contact . [Thesis]. Nanyang Technological University; 2019. Available from: http://hdl.handle.net/10220/48561

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Nanyang Technological University

9. Sailauov, Tolebi. A study of optimization of air traffic network and flight schedules .

Degree: 2019, Nanyang Technological University

 South-East Asia is considered one of the fastest air traffic growing regions in the world. Congested air traffic and weather conditions have thus become major… (more)

Subjects/Keywords: DRNTU::Engineering::Aeronautical engineering::Aviation

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APA (6th Edition):

Sailauov, T. (2019). A study of optimization of air traffic network and flight schedules . (Thesis). Nanyang Technological University. Retrieved from http://hdl.handle.net/10220/48614

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Sailauov, Tolebi. “A study of optimization of air traffic network and flight schedules .” 2019. Thesis, Nanyang Technological University. Accessed January 21, 2020. http://hdl.handle.net/10220/48614.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Sailauov, Tolebi. “A study of optimization of air traffic network and flight schedules .” 2019. Web. 21 Jan 2020.

Vancouver:

Sailauov T. A study of optimization of air traffic network and flight schedules . [Internet] [Thesis]. Nanyang Technological University; 2019. [cited 2020 Jan 21]. Available from: http://hdl.handle.net/10220/48614.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Sailauov T. A study of optimization of air traffic network and flight schedules . [Thesis]. Nanyang Technological University; 2019. Available from: http://hdl.handle.net/10220/48614

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Nanyang Technological University

10. Zhong, Zhiyuan. Numerical investigation on combustion instabilities and its passive control .

Degree: 2012, Nanyang Technological University

 Combustion instabilities are caused by the interaction between unsteady heat releases and acoustic waves. Under certain conditions, the mutual interaction can grow to large oscillations… (more)

Subjects/Keywords: DRNTU::Engineering::Aeronautical engineering

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APA (6th Edition):

Zhong, Z. (2012). Numerical investigation on combustion instabilities and its passive control . (Thesis). Nanyang Technological University. Retrieved from http://hdl.handle.net/10356/50701

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Zhong, Zhiyuan. “Numerical investigation on combustion instabilities and its passive control .” 2012. Thesis, Nanyang Technological University. Accessed January 21, 2020. http://hdl.handle.net/10356/50701.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Zhong, Zhiyuan. “Numerical investigation on combustion instabilities and its passive control .” 2012. Web. 21 Jan 2020.

Vancouver:

Zhong Z. Numerical investigation on combustion instabilities and its passive control . [Internet] [Thesis]. Nanyang Technological University; 2012. [cited 2020 Jan 21]. Available from: http://hdl.handle.net/10356/50701.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Zhong Z. Numerical investigation on combustion instabilities and its passive control . [Thesis]. Nanyang Technological University; 2012. Available from: http://hdl.handle.net/10356/50701

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Nanyang Technological University

11. Zhao, Weihua. Model predictive based UAV formation flight control : formulation, extension and experiment .

Degree: 2012, Nanyang Technological University

 This thesis considers the problem of unmanned aerial vehicle (UAV) formation flight control. This problem has received significant attention recently in the control, robotics and… (more)

Subjects/Keywords: DRNTU::Engineering::Aeronautical engineering

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APA (6th Edition):

Zhao, W. (2012). Model predictive based UAV formation flight control : formulation, extension and experiment . (Thesis). Nanyang Technological University. Retrieved from http://hdl.handle.net/10356/50733

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Zhao, Weihua. “Model predictive based UAV formation flight control : formulation, extension and experiment .” 2012. Thesis, Nanyang Technological University. Accessed January 21, 2020. http://hdl.handle.net/10356/50733.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Zhao, Weihua. “Model predictive based UAV formation flight control : formulation, extension and experiment .” 2012. Web. 21 Jan 2020.

Vancouver:

Zhao W. Model predictive based UAV formation flight control : formulation, extension and experiment . [Internet] [Thesis]. Nanyang Technological University; 2012. [cited 2020 Jan 21]. Available from: http://hdl.handle.net/10356/50733.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Zhao W. Model predictive based UAV formation flight control : formulation, extension and experiment . [Thesis]. Nanyang Technological University; 2012. Available from: http://hdl.handle.net/10356/50733

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Nanyang Technological University

12. Zheng, Yingying. An experimental study on the aerodynamic performance of flexible tandem wings .

Degree: 2016, Nanyang Technological University

 As typical four-wing insects, the dragonflies have the features of both flexible wing and tandem-wing configuration. In previous studies, these two features have been widely… (more)

Subjects/Keywords: DRNTU::Engineering::Aeronautical engineering

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APA (6th Edition):

Zheng, Y. (2016). An experimental study on the aerodynamic performance of flexible tandem wings . (Thesis). Nanyang Technological University. Retrieved from http://hdl.handle.net/10356/66926

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Zheng, Yingying. “An experimental study on the aerodynamic performance of flexible tandem wings .” 2016. Thesis, Nanyang Technological University. Accessed January 21, 2020. http://hdl.handle.net/10356/66926.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Zheng, Yingying. “An experimental study on the aerodynamic performance of flexible tandem wings .” 2016. Web. 21 Jan 2020.

Vancouver:

Zheng Y. An experimental study on the aerodynamic performance of flexible tandem wings . [Internet] [Thesis]. Nanyang Technological University; 2016. [cited 2020 Jan 21]. Available from: http://hdl.handle.net/10356/66926.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Zheng Y. An experimental study on the aerodynamic performance of flexible tandem wings . [Thesis]. Nanyang Technological University; 2016. Available from: http://hdl.handle.net/10356/66926

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

13. Chai, Vincent Wee Sern. Experimental and computational study of flapping wing aerodynamics at low reynolds number .

Degree: 2013, Nanyang Technological University

 Recent rapid developments in micro-sized Unmanned Aerial Vehicles (UAVs) and Underwater Vehicles (UWVs) have attracted renewed research interest in flapping wings aerodynamics. Due to the… (more)

Subjects/Keywords: DRNTU::Engineering::Aeronautical engineering::Aerodynamics

…of flapping wings aerodynamics which involve the complicated kinematic motions and the… …good prediction tool and set of methodologies to describe flapping wings aerodynamics is… …emphasizes the study of aerodynamics of hydrofoil or flat plate which undergoes simplified… …engineer tool for solving engineering problems more effectively. However, most of the… …flapping wings aerodynamics. In summary, this thesis aims to investigate the feasibility of… 

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APA (6th Edition):

Chai, V. W. S. (2013). Experimental and computational study of flapping wing aerodynamics at low reynolds number . (Thesis). Nanyang Technological University. Retrieved from http://hdl.handle.net/10356/54897

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Chai, Vincent Wee Sern. “Experimental and computational study of flapping wing aerodynamics at low reynolds number .” 2013. Thesis, Nanyang Technological University. Accessed January 21, 2020. http://hdl.handle.net/10356/54897.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Chai, Vincent Wee Sern. “Experimental and computational study of flapping wing aerodynamics at low reynolds number .” 2013. Web. 21 Jan 2020.

Vancouver:

Chai VWS. Experimental and computational study of flapping wing aerodynamics at low reynolds number . [Internet] [Thesis]. Nanyang Technological University; 2013. [cited 2020 Jan 21]. Available from: http://hdl.handle.net/10356/54897.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Chai VWS. Experimental and computational study of flapping wing aerodynamics at low reynolds number . [Thesis]. Nanyang Technological University; 2013. Available from: http://hdl.handle.net/10356/54897

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

14. Wang, John Chung Hung. Application of biologically inspired "Pop-Up'' feather style high lift device on micro aerial vehicles.

Degree: 2013, Nanyang Technological University

 Recent years saw the increase in relevance of Micro Aerial Vehicle (MAV) in both civilian and military applications. One of the more attractive feature of… (more)

Subjects/Keywords: DRNTU::Engineering::Aeronautical engineering::Aerodynamics

aerodynamics constants were measured using pressure tap installed on the airfoil model, and recorded… …platform. The raw data and aerodynamics coefficients can be exported in comma-separated-value… …the flap has been shown to have no significant effect on the aerodynamics property of the… 

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APA (6th Edition):

Wang, J. C. H. (2013). Application of biologically inspired "Pop-Up'' feather style high lift device on micro aerial vehicles. (Thesis). Nanyang Technological University. Retrieved from http://hdl.handle.net/10356/55002

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Wang, John Chung Hung. “Application of biologically inspired "Pop-Up'' feather style high lift device on micro aerial vehicles. ” 2013. Thesis, Nanyang Technological University. Accessed January 21, 2020. http://hdl.handle.net/10356/55002.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Wang, John Chung Hung. “Application of biologically inspired "Pop-Up'' feather style high lift device on micro aerial vehicles. ” 2013. Web. 21 Jan 2020.

Vancouver:

Wang JCH. Application of biologically inspired "Pop-Up'' feather style high lift device on micro aerial vehicles. [Internet] [Thesis]. Nanyang Technological University; 2013. [cited 2020 Jan 21]. Available from: http://hdl.handle.net/10356/55002.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Wang JCH. Application of biologically inspired "Pop-Up'' feather style high lift device on micro aerial vehicles. [Thesis]. Nanyang Technological University; 2013. Available from: http://hdl.handle.net/10356/55002

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

15. Xiang, Junting. Miniature gas turbines : numerical study of the effects of miniaturization on the performance of compressor .

Degree: 2015, Nanyang Technological University

 Micro Gas Turbines (MGT) are an attractive choice for Unmanned Aerial Vehicles (UAV) and small-scale power generation. Compared with other propulsion systems, MGT have several… (more)

Subjects/Keywords: DRNTU::Engineering::Aeronautical engineering::Aerodynamics

engineering guidance. Although extensive investigations regarding heat transfer effect on gas… 

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APA (6th Edition):

Xiang, J. (2015). Miniature gas turbines : numerical study of the effects of miniaturization on the performance of compressor . (Thesis). Nanyang Technological University. Retrieved from http://hdl.handle.net/10356/65179

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Xiang, Junting. “Miniature gas turbines : numerical study of the effects of miniaturization on the performance of compressor .” 2015. Thesis, Nanyang Technological University. Accessed January 21, 2020. http://hdl.handle.net/10356/65179.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Xiang, Junting. “Miniature gas turbines : numerical study of the effects of miniaturization on the performance of compressor .” 2015. Web. 21 Jan 2020.

Vancouver:

Xiang J. Miniature gas turbines : numerical study of the effects of miniaturization on the performance of compressor . [Internet] [Thesis]. Nanyang Technological University; 2015. [cited 2020 Jan 21]. Available from: http://hdl.handle.net/10356/65179.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Xiang J. Miniature gas turbines : numerical study of the effects of miniaturization on the performance of compressor . [Thesis]. Nanyang Technological University; 2015. Available from: http://hdl.handle.net/10356/65179

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Nanyang Technological University

16. Adnan Maqsood. Longitudinal dynamics, optimization and control of aircraft transition maneuver using aerodynamic vectoring .

Degree: 2012, Nanyang Technological University

 In order to enhance the flight envelope of Unmanned Air Vehicles (UAVs), there have been efforts to combine the excellent hover capabilities of rotorcraft with… (more)

Subjects/Keywords: DRNTU::Engineering::Aeronautical engineering::Aircraft; DRNTU::Engineering::Aeronautical engineering::Flight simulation

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APA (6th Edition):

Maqsood, A. (2012). Longitudinal dynamics, optimization and control of aircraft transition maneuver using aerodynamic vectoring . (Thesis). Nanyang Technological University. Retrieved from http://hdl.handle.net/10356/48041

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Maqsood, Adnan. “Longitudinal dynamics, optimization and control of aircraft transition maneuver using aerodynamic vectoring .” 2012. Thesis, Nanyang Technological University. Accessed January 21, 2020. http://hdl.handle.net/10356/48041.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Maqsood, Adnan. “Longitudinal dynamics, optimization and control of aircraft transition maneuver using aerodynamic vectoring .” 2012. Web. 21 Jan 2020.

Vancouver:

Maqsood A. Longitudinal dynamics, optimization and control of aircraft transition maneuver using aerodynamic vectoring . [Internet] [Thesis]. Nanyang Technological University; 2012. [cited 2020 Jan 21]. Available from: http://hdl.handle.net/10356/48041.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Maqsood A. Longitudinal dynamics, optimization and control of aircraft transition maneuver using aerodynamic vectoring . [Thesis]. Nanyang Technological University; 2012. Available from: http://hdl.handle.net/10356/48041

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

17. Yogeshwaran Jayaraman. Dynamics models of flexible aircraft .

Degree: 2014, Nanyang Technological University

 Recent trends in aircraft design owing to requirements of high performance and weight reduction have resulted in aircraft possessing significant structural flexibility. Under these conditions,… (more)

Subjects/Keywords: DRNTU::Engineering::Aeronautical engineering::Flight simulation; DRNTU::Engineering::Aeronautical engineering::Aircraft

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APA (6th Edition):

Jayaraman, Y. (2014). Dynamics models of flexible aircraft . (Thesis). Nanyang Technological University. Retrieved from http://hdl.handle.net/10356/61444

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Jayaraman, Yogeshwaran. “Dynamics models of flexible aircraft .” 2014. Thesis, Nanyang Technological University. Accessed January 21, 2020. http://hdl.handle.net/10356/61444.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Jayaraman, Yogeshwaran. “Dynamics models of flexible aircraft .” 2014. Web. 21 Jan 2020.

Vancouver:

Jayaraman Y. Dynamics models of flexible aircraft . [Internet] [Thesis]. Nanyang Technological University; 2014. [cited 2020 Jan 21]. Available from: http://hdl.handle.net/10356/61444.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Jayaraman Y. Dynamics models of flexible aircraft . [Thesis]. Nanyang Technological University; 2014. Available from: http://hdl.handle.net/10356/61444

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Nanyang Technological University

18. Xie, Zhen. Forecasting, visibility and 3D route optimization for future air traffic management .

Degree: 2018, Nanyang Technological University

 Based on time-series Recurrent Neural Network (RNN) forecasting results, air traffic volumes and air passenger volumes will keep increasing for the coming decades. It will… (more)

Subjects/Keywords: DRNTU::Engineering::Aeronautical engineering::Flight simulation

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APA (6th Edition):

Xie, Z. (2018). Forecasting, visibility and 3D route optimization for future air traffic management . (Thesis). Nanyang Technological University. Retrieved from http://hdl.handle.net/10220/45896

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Xie, Zhen. “Forecasting, visibility and 3D route optimization for future air traffic management .” 2018. Thesis, Nanyang Technological University. Accessed January 21, 2020. http://hdl.handle.net/10220/45896.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Xie, Zhen. “Forecasting, visibility and 3D route optimization for future air traffic management .” 2018. Web. 21 Jan 2020.

Vancouver:

Xie Z. Forecasting, visibility and 3D route optimization for future air traffic management . [Internet] [Thesis]. Nanyang Technological University; 2018. [cited 2020 Jan 21]. Available from: http://hdl.handle.net/10220/45896.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Xie Z. Forecasting, visibility and 3D route optimization for future air traffic management . [Thesis]. Nanyang Technological University; 2018. Available from: http://hdl.handle.net/10220/45896

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Nanyang Technological University

19. Wan, Chao. Mixing enhancement in jet flow using the air tab technique .

Degree: 2012, Nanyang Technological University

 It is well known that the triangular tab is an effective device to enhance jet’s mixing. However, due to its protrusion nature, its blockage will… (more)

Subjects/Keywords: DRNTU::Engineering::Aeronautical engineering::Jet propulsion

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APA (6th Edition):

Wan, C. (2012). Mixing enhancement in jet flow using the air tab technique . (Thesis). Nanyang Technological University. Retrieved from http://hdl.handle.net/10356/50794

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Wan, Chao. “Mixing enhancement in jet flow using the air tab technique .” 2012. Thesis, Nanyang Technological University. Accessed January 21, 2020. http://hdl.handle.net/10356/50794.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Wan, Chao. “Mixing enhancement in jet flow using the air tab technique .” 2012. Web. 21 Jan 2020.

Vancouver:

Wan C. Mixing enhancement in jet flow using the air tab technique . [Internet] [Thesis]. Nanyang Technological University; 2012. [cited 2020 Jan 21]. Available from: http://hdl.handle.net/10356/50794.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Wan C. Mixing enhancement in jet flow using the air tab technique . [Thesis]. Nanyang Technological University; 2012. Available from: http://hdl.handle.net/10356/50794

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Nanyang Technological University

20. Sun, Hui. An integrated microfludic chip with continuous flow centrifugation for sample concentration, particle collestion and particle transport .

Degree: 2010, Nanyang Technological University

 Biological sample concentration in a large volume is essential to bio-analyses of environmental samples. If particles in drinking water can be high-throughput concentrated, collected and… (more)

Subjects/Keywords: DRNTU::Engineering::Aeronautical engineering; DRNTU::Engineering::Mechanical engineering

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APA (6th Edition):

Sun, H. (2010). An integrated microfludic chip with continuous flow centrifugation for sample concentration, particle collestion and particle transport . (Thesis). Nanyang Technological University. Retrieved from http://hdl.handle.net/10356/47126

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Sun, Hui. “An integrated microfludic chip with continuous flow centrifugation for sample concentration, particle collestion and particle transport .” 2010. Thesis, Nanyang Technological University. Accessed January 21, 2020. http://hdl.handle.net/10356/47126.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Sun, Hui. “An integrated microfludic chip with continuous flow centrifugation for sample concentration, particle collestion and particle transport .” 2010. Web. 21 Jan 2020.

Vancouver:

Sun H. An integrated microfludic chip with continuous flow centrifugation for sample concentration, particle collestion and particle transport . [Internet] [Thesis]. Nanyang Technological University; 2010. [cited 2020 Jan 21]. Available from: http://hdl.handle.net/10356/47126.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Sun H. An integrated microfludic chip with continuous flow centrifugation for sample concentration, particle collestion and particle transport . [Thesis]. Nanyang Technological University; 2010. Available from: http://hdl.handle.net/10356/47126

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Nanyang Technological University

21. Sreekanth Kandammathe Valiyaveedu. Investigations into plasmonic lithography concepts for high resolution nanoscale feature patterning .

Degree: 2012, Nanyang Technological University

 Plasmonic lithography, which is not restricted by free space diffraction limit, is one of the potential research thrust areas as it offers the possibility for… (more)

Subjects/Keywords: DRNTU::Engineering::Mechanical engineering; DRNTU::Engineering::Aeronautical engineering

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APA (6th Edition):

Valiyaveedu, S. K. (2012). Investigations into plasmonic lithography concepts for high resolution nanoscale feature patterning . (Thesis). Nanyang Technological University. Retrieved from http://hdl.handle.net/10356/48682

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Valiyaveedu, Sreekanth Kandammathe. “Investigations into plasmonic lithography concepts for high resolution nanoscale feature patterning .” 2012. Thesis, Nanyang Technological University. Accessed January 21, 2020. http://hdl.handle.net/10356/48682.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Valiyaveedu, Sreekanth Kandammathe. “Investigations into plasmonic lithography concepts for high resolution nanoscale feature patterning .” 2012. Web. 21 Jan 2020.

Vancouver:

Valiyaveedu SK. Investigations into plasmonic lithography concepts for high resolution nanoscale feature patterning . [Internet] [Thesis]. Nanyang Technological University; 2012. [cited 2020 Jan 21]. Available from: http://hdl.handle.net/10356/48682.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Valiyaveedu SK. Investigations into plasmonic lithography concepts for high resolution nanoscale feature patterning . [Thesis]. Nanyang Technological University; 2012. Available from: http://hdl.handle.net/10356/48682

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Nanyang Technological University

22. Gou, Liangliang. A first-principle study on lattice properties and atom positions of TiNiCu shape memory alloys .

Degree: 2016, Nanyang Technological University

 Since its discovery, TiNi-based shape memory alloys (SMAs) have attracted much attention and have spawned various innovative applications in the biomedical, aerospace, robotic and automotive… (more)

Subjects/Keywords: DRNTU::Engineering::Mechanical engineering; DRNTU::Engineering::Aeronautical engineering

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APA (6th Edition):

Gou, L. (2016). A first-principle study on lattice properties and atom positions of TiNiCu shape memory alloys . (Thesis). Nanyang Technological University. Retrieved from http://hdl.handle.net/10356/68525

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Gou, Liangliang. “A first-principle study on lattice properties and atom positions of TiNiCu shape memory alloys .” 2016. Thesis, Nanyang Technological University. Accessed January 21, 2020. http://hdl.handle.net/10356/68525.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Gou, Liangliang. “A first-principle study on lattice properties and atom positions of TiNiCu shape memory alloys .” 2016. Web. 21 Jan 2020.

Vancouver:

Gou L. A first-principle study on lattice properties and atom positions of TiNiCu shape memory alloys . [Internet] [Thesis]. Nanyang Technological University; 2016. [cited 2020 Jan 21]. Available from: http://hdl.handle.net/10356/68525.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Gou L. A first-principle study on lattice properties and atom positions of TiNiCu shape memory alloys . [Thesis]. Nanyang Technological University; 2016. Available from: http://hdl.handle.net/10356/68525

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Nanyang Technological University

23. Sudarshan, Vidya. An integrated index to detect the extent of myocardial infarction using echocardiographic texture analysis .

Degree: 2016, Nanyang Technological University

 Expansion of infarcted zone after Myocardial Infarction (MI) has serious short and long-term consequences and contributes to increased mortality. Early detection and quantitative assessment of… (more)

Subjects/Keywords: DRNTU::Engineering::Mechanical engineering; DRNTU::Engineering::Aeronautical engineering

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APA (6th Edition):

Sudarshan, V. (2016). An integrated index to detect the extent of myocardial infarction using echocardiographic texture analysis . (Thesis). Nanyang Technological University. Retrieved from http://hdl.handle.net/10356/68773

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Sudarshan, Vidya. “An integrated index to detect the extent of myocardial infarction using echocardiographic texture analysis .” 2016. Thesis, Nanyang Technological University. Accessed January 21, 2020. http://hdl.handle.net/10356/68773.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Sudarshan, Vidya. “An integrated index to detect the extent of myocardial infarction using echocardiographic texture analysis .” 2016. Web. 21 Jan 2020.

Vancouver:

Sudarshan V. An integrated index to detect the extent of myocardial infarction using echocardiographic texture analysis . [Internet] [Thesis]. Nanyang Technological University; 2016. [cited 2020 Jan 21]. Available from: http://hdl.handle.net/10356/68773.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Sudarshan V. An integrated index to detect the extent of myocardial infarction using echocardiographic texture analysis . [Thesis]. Nanyang Technological University; 2016. Available from: http://hdl.handle.net/10356/68773

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

24. Pey, Yin Yin. Analysis of flow structures in cavity flow with modifications to cavity geometry .

Degree: 2014, Nanyang Technological University

 Flow over cavity exists in a wide range of flow phenomena and remains a challenging problem till today. The objective of this study is to… (more)

Subjects/Keywords: DRNTU::Engineering::Aeronautical engineering; DRNTU::Engineering::Mechanical engineering; DRNTU::Engineering::Mechanical engineering::Fluid mechanics; DRNTU::Engineering::Aeronautical engineering::Aerodynamics

…the fundamental flow within the cavity. This could be useful for engineering applications… …engineering applications of cavity and the fundamentals of flow physics within cavity. Since most… …of passive flow control. For engineering applications, pressure measurements will be taken… …works) Implementation of trailing edge ramps Engineering Applications (pressure… 

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APA (6th Edition):

Pey, Y. Y. (2014). Analysis of flow structures in cavity flow with modifications to cavity geometry . (Thesis). Nanyang Technological University. Retrieved from http://hdl.handle.net/10356/59862

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Pey, Yin Yin. “Analysis of flow structures in cavity flow with modifications to cavity geometry .” 2014. Thesis, Nanyang Technological University. Accessed January 21, 2020. http://hdl.handle.net/10356/59862.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Pey, Yin Yin. “Analysis of flow structures in cavity flow with modifications to cavity geometry .” 2014. Web. 21 Jan 2020.

Vancouver:

Pey YY. Analysis of flow structures in cavity flow with modifications to cavity geometry . [Internet] [Thesis]. Nanyang Technological University; 2014. [cited 2020 Jan 21]. Available from: http://hdl.handle.net/10356/59862.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Pey YY. Analysis of flow structures in cavity flow with modifications to cavity geometry . [Thesis]. Nanyang Technological University; 2014. Available from: http://hdl.handle.net/10356/59862

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Nanyang Technological University

25. Tan, Chun Kiat. Ship deck landing of multi-rotor unmanned aerial vehicle .

Degree: 2016, Nanyang Technological University

 The ship deck landing problem of a multi-rotor UAV is solved in this thesis. This problem is divided into tracking and landing sub-problems. In the… (more)

Subjects/Keywords: DRNTU::Engineering::Electrical and electronic engineering::Control and instrumentation::Control engineering; DRNTU::Engineering::Aeronautical engineering

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APA (6th Edition):

Tan, C. K. (2016). Ship deck landing of multi-rotor unmanned aerial vehicle . (Thesis). Nanyang Technological University. Retrieved from http://hdl.handle.net/10356/66721

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Tan, Chun Kiat. “Ship deck landing of multi-rotor unmanned aerial vehicle .” 2016. Thesis, Nanyang Technological University. Accessed January 21, 2020. http://hdl.handle.net/10356/66721.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Tan, Chun Kiat. “Ship deck landing of multi-rotor unmanned aerial vehicle .” 2016. Web. 21 Jan 2020.

Vancouver:

Tan CK. Ship deck landing of multi-rotor unmanned aerial vehicle . [Internet] [Thesis]. Nanyang Technological University; 2016. [cited 2020 Jan 21]. Available from: http://hdl.handle.net/10356/66721.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Tan CK. Ship deck landing of multi-rotor unmanned aerial vehicle . [Thesis]. Nanyang Technological University; 2016. Available from: http://hdl.handle.net/10356/66721

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Nanyang Technological University

26. Zhu, Senqiang. Target tracking and source seeking using unmanned aerial vehicles with input constraints .

Degree: 2014, Nanyang Technological University

 The potential applications of unmanned aerial vehicles (UAVs) in both military and civilian fields have spurred the research on UAV control. Although great progresses in… (more)

Subjects/Keywords: DRNTU::Engineering::Aeronautical engineering; DRNTU::Engineering::Electrical and electronic engineering::Control and instrumentation::Robotics

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APA (6th Edition):

Zhu, S. (2014). Target tracking and source seeking using unmanned aerial vehicles with input constraints . (Thesis). Nanyang Technological University. Retrieved from http://hdl.handle.net/10356/59961

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Zhu, Senqiang. “Target tracking and source seeking using unmanned aerial vehicles with input constraints .” 2014. Thesis, Nanyang Technological University. Accessed January 21, 2020. http://hdl.handle.net/10356/59961.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Zhu, Senqiang. “Target tracking and source seeking using unmanned aerial vehicles with input constraints .” 2014. Web. 21 Jan 2020.

Vancouver:

Zhu S. Target tracking and source seeking using unmanned aerial vehicles with input constraints . [Internet] [Thesis]. Nanyang Technological University; 2014. [cited 2020 Jan 21]. Available from: http://hdl.handle.net/10356/59961.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Zhu S. Target tracking and source seeking using unmanned aerial vehicles with input constraints . [Thesis]. Nanyang Technological University; 2014. Available from: http://hdl.handle.net/10356/59961

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Nanyang Technological University

27. Koh, Alan Fu Hai. Approximating conditions within a multistage axial compressor and assessing the possibility of hot surface ignition on the heated surfaces .

Degree: 2018, Nanyang Technological University

 Aero-derivative gas turbines are deployed on offshore oil and gas production platforms, among other engine types and locations relevant to the industry. These gas turbines… (more)

Subjects/Keywords: DRNTU::Engineering::Aeronautical engineering::Aircraft motors and engines

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APA (6th Edition):

Koh, A. F. H. (2018). Approximating conditions within a multistage axial compressor and assessing the possibility of hot surface ignition on the heated surfaces . (Thesis). Nanyang Technological University. Retrieved from http://hdl.handle.net/10220/46287

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Koh, Alan Fu Hai. “Approximating conditions within a multistage axial compressor and assessing the possibility of hot surface ignition on the heated surfaces .” 2018. Thesis, Nanyang Technological University. Accessed January 21, 2020. http://hdl.handle.net/10220/46287.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Koh, Alan Fu Hai. “Approximating conditions within a multistage axial compressor and assessing the possibility of hot surface ignition on the heated surfaces .” 2018. Web. 21 Jan 2020.

Vancouver:

Koh AFH. Approximating conditions within a multistage axial compressor and assessing the possibility of hot surface ignition on the heated surfaces . [Internet] [Thesis]. Nanyang Technological University; 2018. [cited 2020 Jan 21]. Available from: http://hdl.handle.net/10220/46287.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Koh AFH. Approximating conditions within a multistage axial compressor and assessing the possibility of hot surface ignition on the heated surfaces . [Thesis]. Nanyang Technological University; 2018. Available from: http://hdl.handle.net/10220/46287

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Nanyang Technological University

28. Wong, Yoke Rung. Development of a real time quality monitoring device for resistance spot welding .

Degree: 2008, Nanyang Technological University

Electrical input impedance is used as a new monitoring signature to study its correlation between RSW process and micro structural changes of RSW so that a real time quality monitoring device can be achieved with help of automated tools such as Artificial Neural Network.

Subjects/Keywords: DRNTU::Engineering::Aeronautical engineering

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Wong, Y. R. (2008). Development of a real time quality monitoring device for resistance spot welding . (Thesis). Nanyang Technological University. Retrieved from http://hdl.handle.net/10356/5395

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Wong, Yoke Rung. “Development of a real time quality monitoring device for resistance spot welding .” 2008. Thesis, Nanyang Technological University. Accessed January 21, 2020. http://hdl.handle.net/10356/5395.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Wong, Yoke Rung. “Development of a real time quality monitoring device for resistance spot welding .” 2008. Web. 21 Jan 2020.

Vancouver:

Wong YR. Development of a real time quality monitoring device for resistance spot welding . [Internet] [Thesis]. Nanyang Technological University; 2008. [cited 2020 Jan 21]. Available from: http://hdl.handle.net/10356/5395.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Wong YR. Development of a real time quality monitoring device for resistance spot welding . [Thesis]. Nanyang Technological University; 2008. Available from: http://hdl.handle.net/10356/5395

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Nanyang Technological University

29. Seow, Aik Khiam. Design, fabrication, evaluation of low-speed UAV wing flap actuated with shape memory alloy .

Degree: 2009, Nanyang Technological University

 The novel properties of shape memory alloys (SMA) are very attractive for providing new solutions to challenging problems in aerospace engineering. Although SMA possess very… (more)

Subjects/Keywords: DRNTU::Engineering::Aeronautical engineering::Aircraft

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Seow, A. K. (2009). Design, fabrication, evaluation of low-speed UAV wing flap actuated with shape memory alloy . (Thesis). Nanyang Technological University. Retrieved from http://hdl.handle.net/10356/18669

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Seow, Aik Khiam. “Design, fabrication, evaluation of low-speed UAV wing flap actuated with shape memory alloy .” 2009. Thesis, Nanyang Technological University. Accessed January 21, 2020. http://hdl.handle.net/10356/18669.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Seow, Aik Khiam. “Design, fabrication, evaluation of low-speed UAV wing flap actuated with shape memory alloy .” 2009. Web. 21 Jan 2020.

Vancouver:

Seow AK. Design, fabrication, evaluation of low-speed UAV wing flap actuated with shape memory alloy . [Internet] [Thesis]. Nanyang Technological University; 2009. [cited 2020 Jan 21]. Available from: http://hdl.handle.net/10356/18669.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Seow AK. Design, fabrication, evaluation of low-speed UAV wing flap actuated with shape memory alloy . [Thesis]. Nanyang Technological University; 2009. Available from: http://hdl.handle.net/10356/18669

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Nanyang Technological University

30. Setiawan, Suhartono. Design, flight dynamic analysis and hover control of a vertical take-off and landing micro air vehicle .

Degree: 2009, Nanyang Technological University

 A ducted fan Vertical Take-off and Landing (VTOL) Micro Air Vehicle (MAV) is developed. The vehicle is equipped with a wing that can be rotated… (more)

Subjects/Keywords: DRNTU::Engineering::Aeronautical engineering::Aircraft

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Setiawan, S. (2009). Design, flight dynamic analysis and hover control of a vertical take-off and landing micro air vehicle . (Thesis). Nanyang Technological University. Retrieved from http://hdl.handle.net/10356/19010

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Setiawan, Suhartono. “Design, flight dynamic analysis and hover control of a vertical take-off and landing micro air vehicle .” 2009. Thesis, Nanyang Technological University. Accessed January 21, 2020. http://hdl.handle.net/10356/19010.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Setiawan, Suhartono. “Design, flight dynamic analysis and hover control of a vertical take-off and landing micro air vehicle .” 2009. Web. 21 Jan 2020.

Vancouver:

Setiawan S. Design, flight dynamic analysis and hover control of a vertical take-off and landing micro air vehicle . [Internet] [Thesis]. Nanyang Technological University; 2009. [cited 2020 Jan 21]. Available from: http://hdl.handle.net/10356/19010.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Setiawan S. Design, flight dynamic analysis and hover control of a vertical take-off and landing micro air vehicle . [Thesis]. Nanyang Technological University; 2009. Available from: http://hdl.handle.net/10356/19010

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

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