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You searched for subject:(helicopter). Showing records 1 – 30 of 442 total matches.

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Penn State University

1. Walsh, Gregory Daniel. A PRELIMINARY ACOUSTIC INVESTIGATION OF A COAXIAL HELICOPTER IN HIGH-SPEED FLIGHT.

Degree: 2016, Penn State University

 The desire for a vertical takeoff and landing (VTOL) aircraft capable of high forward flight speeds is very strong. Compound lift-offset coaxial helicopter designs have… (more)

Subjects/Keywords: Acoustics; Coaxial Helicopter; Rotorcraft; Rotorcraft Acoustics; Helicopter

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APA (6th Edition):

Walsh, G. D. (2016). A PRELIMINARY ACOUSTIC INVESTIGATION OF A COAXIAL HELICOPTER IN HIGH-SPEED FLIGHT. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/c534fn92g

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):

Walsh, Gregory Daniel. “A PRELIMINARY ACOUSTIC INVESTIGATION OF A COAXIAL HELICOPTER IN HIGH-SPEED FLIGHT.” 2016. Thesis, Penn State University. Accessed April 21, 2021. https://submit-etda.libraries.psu.edu/catalog/c534fn92g.

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

MLA Handbook (7th Edition):

Walsh, Gregory Daniel. “A PRELIMINARY ACOUSTIC INVESTIGATION OF A COAXIAL HELICOPTER IN HIGH-SPEED FLIGHT.” 2016. Web. 21 Apr 2021.

Vancouver:

Walsh GD. A PRELIMINARY ACOUSTIC INVESTIGATION OF A COAXIAL HELICOPTER IN HIGH-SPEED FLIGHT. [Internet] [Thesis]. Penn State University; 2016. [cited 2021 Apr 21]. Available from: https://submit-etda.libraries.psu.edu/catalog/c534fn92g.

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

Council of Science Editors:

Walsh GD. A PRELIMINARY ACOUSTIC INVESTIGATION OF A COAXIAL HELICOPTER IN HIGH-SPEED FLIGHT. [Thesis]. Penn State University; 2016. Available from: https://submit-etda.libraries.psu.edu/catalog/c534fn92g

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


California State University – Chico

2. Jia, Yitao. A multi-input multi-output self tuning regulator for nonlinear helicopter control .

Degree: 2013, California State University – Chico

 This project aims at designing an on-line controller in the form of a Multi Input Multi Output Self Tuning Regulator, to stabilize a 6 degree… (more)

Subjects/Keywords: nonlinear helicopter control

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APA (6th Edition):

Jia, Y. (2013). A multi-input multi-output self tuning regulator for nonlinear helicopter control . (Thesis). California State University – Chico. Retrieved from http://hdl.handle.net/10211.4/602

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):

Jia, Yitao. “A multi-input multi-output self tuning regulator for nonlinear helicopter control .” 2013. Thesis, California State University – Chico. Accessed April 21, 2021. http://hdl.handle.net/10211.4/602.

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

MLA Handbook (7th Edition):

Jia, Yitao. “A multi-input multi-output self tuning regulator for nonlinear helicopter control .” 2013. Web. 21 Apr 2021.

Vancouver:

Jia Y. A multi-input multi-output self tuning regulator for nonlinear helicopter control . [Internet] [Thesis]. California State University – Chico; 2013. [cited 2021 Apr 21]. Available from: http://hdl.handle.net/10211.4/602.

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

Council of Science Editors:

Jia Y. A multi-input multi-output self tuning regulator for nonlinear helicopter control . [Thesis]. California State University – Chico; 2013. Available from: http://hdl.handle.net/10211.4/602

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


Delft University of Technology

3. Declerck, Laurent (author). Feasibility Study of a Load Alleviation Strategy on a Compound Helicopter Using Redundant Controls.

Degree: 2019, Delft University of Technology

 <p class="MsoNormal">The compound helicopter gains interest as operational needs push future rotorcraft capabilities beyond current standards. The compound helicopter is investigated as part of the… (more)

Subjects/Keywords: Structural Load Alleviation; SLA; Compound Helicopter; Helicopter; Helicopter Model; Rotor; Flapping Dynamics; Blade Flap

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APA (6th Edition):

Declerck, L. (. (2019). Feasibility Study of a Load Alleviation Strategy on a Compound Helicopter Using Redundant Controls. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:b96a69b6-7aac-436d-a2e6-d3b878d14761

Chicago Manual of Style (16th Edition):

Declerck, Laurent (author). “Feasibility Study of a Load Alleviation Strategy on a Compound Helicopter Using Redundant Controls.” 2019. Masters Thesis, Delft University of Technology. Accessed April 21, 2021. http://resolver.tudelft.nl/uuid:b96a69b6-7aac-436d-a2e6-d3b878d14761.

MLA Handbook (7th Edition):

Declerck, Laurent (author). “Feasibility Study of a Load Alleviation Strategy on a Compound Helicopter Using Redundant Controls.” 2019. Web. 21 Apr 2021.

Vancouver:

Declerck L(. Feasibility Study of a Load Alleviation Strategy on a Compound Helicopter Using Redundant Controls. [Internet] [Masters thesis]. Delft University of Technology; 2019. [cited 2021 Apr 21]. Available from: http://resolver.tudelft.nl/uuid:b96a69b6-7aac-436d-a2e6-d3b878d14761.

Council of Science Editors:

Declerck L(. Feasibility Study of a Load Alleviation Strategy on a Compound Helicopter Using Redundant Controls. [Masters Thesis]. Delft University of Technology; 2019. Available from: http://resolver.tudelft.nl/uuid:b96a69b6-7aac-436d-a2e6-d3b878d14761


University of Alberta

4. Godbolt, Bryan M. Experimental Nonlinear Control of a Helicopter Unmanned Aerial Vehicle (UAV).

Degree: PhD, Department of Electrical and Computer Engineering, 2013, University of Alberta

Helicopter Unmanned Aerial Vehicles (UAVs) present a challenging control problem since their dynamics are nonlinear, underactuated and non-minimum phase. Although it is inherently an applied… (more)

Subjects/Keywords: helicopter; control theory; unmanned vehicles

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APA (6th Edition):

Godbolt, B. M. (2013). Experimental Nonlinear Control of a Helicopter Unmanned Aerial Vehicle (UAV). (Doctoral Dissertation). University of Alberta. Retrieved from https://era.library.ualberta.ca/files/vd66w1412

Chicago Manual of Style (16th Edition):

Godbolt, Bryan M. “Experimental Nonlinear Control of a Helicopter Unmanned Aerial Vehicle (UAV).” 2013. Doctoral Dissertation, University of Alberta. Accessed April 21, 2021. https://era.library.ualberta.ca/files/vd66w1412.

MLA Handbook (7th Edition):

Godbolt, Bryan M. “Experimental Nonlinear Control of a Helicopter Unmanned Aerial Vehicle (UAV).” 2013. Web. 21 Apr 2021.

Vancouver:

Godbolt BM. Experimental Nonlinear Control of a Helicopter Unmanned Aerial Vehicle (UAV). [Internet] [Doctoral dissertation]. University of Alberta; 2013. [cited 2021 Apr 21]. Available from: https://era.library.ualberta.ca/files/vd66w1412.

Council of Science Editors:

Godbolt BM. Experimental Nonlinear Control of a Helicopter Unmanned Aerial Vehicle (UAV). [Doctoral Dissertation]. University of Alberta; 2013. Available from: https://era.library.ualberta.ca/files/vd66w1412

5. Shashidhara T. Modeling and analysis of helicopter vibrations during dynamic conditions;.

Degree: Mechanical engineering, 2014, Kuvempu University

With increasing demand for passenger transportation and demand for high speed and high performance helicopters for defense vibration control has become an important design objective… (more)

Subjects/Keywords: Helicopter vibrations- Modeling; Mechanical engineering

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APA (6th Edition):

T, S. (2014). Modeling and analysis of helicopter vibrations during dynamic conditions;. (Thesis). Kuvempu University. Retrieved from http://shodhganga.inflibnet.ac.in/handle/10603/20337

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):

T, Shashidhara. “Modeling and analysis of helicopter vibrations during dynamic conditions;.” 2014. Thesis, Kuvempu University. Accessed April 21, 2021. http://shodhganga.inflibnet.ac.in/handle/10603/20337.

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

MLA Handbook (7th Edition):

T, Shashidhara. “Modeling and analysis of helicopter vibrations during dynamic conditions;.” 2014. Web. 21 Apr 2021.

Vancouver:

T S. Modeling and analysis of helicopter vibrations during dynamic conditions;. [Internet] [Thesis]. Kuvempu University; 2014. [cited 2021 Apr 21]. Available from: http://shodhganga.inflibnet.ac.in/handle/10603/20337.

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

Council of Science Editors:

T S. Modeling and analysis of helicopter vibrations during dynamic conditions;. [Thesis]. Kuvempu University; 2014. Available from: http://shodhganga.inflibnet.ac.in/handle/10603/20337

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


Texas A&M University

6. Taylor, Bradley Whitten. Experimental Investigation of Helicopter Weight and Mass Center Estimation.

Degree: MS, Aerospace Engineering, 2013, Texas A&M University

 Real-time estimates of weight and mass center location for helicopters are desirable for flight control and condition-based maintenance purposes. While methods to estimate mass parameters… (more)

Subjects/Keywords: Helicopter; Weight; Mass Center; Estimation

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APA (6th Edition):

Taylor, B. W. (2013). Experimental Investigation of Helicopter Weight and Mass Center Estimation. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/149488

Chicago Manual of Style (16th Edition):

Taylor, Bradley Whitten. “Experimental Investigation of Helicopter Weight and Mass Center Estimation.” 2013. Masters Thesis, Texas A&M University. Accessed April 21, 2021. http://hdl.handle.net/1969.1/149488.

MLA Handbook (7th Edition):

Taylor, Bradley Whitten. “Experimental Investigation of Helicopter Weight and Mass Center Estimation.” 2013. Web. 21 Apr 2021.

Vancouver:

Taylor BW. Experimental Investigation of Helicopter Weight and Mass Center Estimation. [Internet] [Masters thesis]. Texas A&M University; 2013. [cited 2021 Apr 21]. Available from: http://hdl.handle.net/1969.1/149488.

Council of Science Editors:

Taylor BW. Experimental Investigation of Helicopter Weight and Mass Center Estimation. [Masters Thesis]. Texas A&M University; 2013. Available from: http://hdl.handle.net/1969.1/149488


Delft University of Technology

7. Jonkheijm, Laurens (author). Predicting helicopter damage caused by a collision with an Unmanned Aerial System using explicit Finite Element Analysis.

Degree: 2020, Delft University of Technology

Due to an exponential growth in the number of shipments of Unmanned Aerial Systems (UAS), the amount of these devices operating in the sky has… (more)

Subjects/Keywords: UAS; impact; helicopter; damage

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APA (6th Edition):

Jonkheijm, L. (. (2020). Predicting helicopter damage caused by a collision with an Unmanned Aerial System using explicit Finite Element Analysis. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:90105518-e3f8-4355-b9d3-bf541215e83c

Chicago Manual of Style (16th Edition):

Jonkheijm, Laurens (author). “Predicting helicopter damage caused by a collision with an Unmanned Aerial System using explicit Finite Element Analysis.” 2020. Masters Thesis, Delft University of Technology. Accessed April 21, 2021. http://resolver.tudelft.nl/uuid:90105518-e3f8-4355-b9d3-bf541215e83c.

MLA Handbook (7th Edition):

Jonkheijm, Laurens (author). “Predicting helicopter damage caused by a collision with an Unmanned Aerial System using explicit Finite Element Analysis.” 2020. Web. 21 Apr 2021.

Vancouver:

Jonkheijm L(. Predicting helicopter damage caused by a collision with an Unmanned Aerial System using explicit Finite Element Analysis. [Internet] [Masters thesis]. Delft University of Technology; 2020. [cited 2021 Apr 21]. Available from: http://resolver.tudelft.nl/uuid:90105518-e3f8-4355-b9d3-bf541215e83c.

Council of Science Editors:

Jonkheijm L(. Predicting helicopter damage caused by a collision with an Unmanned Aerial System using explicit Finite Element Analysis. [Masters Thesis]. Delft University of Technology; 2020. Available from: http://resolver.tudelft.nl/uuid:90105518-e3f8-4355-b9d3-bf541215e83c


University of Manchester

8. Zhang, Lin. Control strategies and stability analysis of small-scale unmanned helicopters.

Degree: PhD, 2017, University of Manchester

 This thesis presents the design and the stability analysis of a hierarchical controller for unmanned aerial vehicles. We utilize non-linear control methodology to command dynamics… (more)

Subjects/Keywords: 629.133; two-time scale; helicopter

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APA (6th Edition):

Zhang, L. (2017). Control strategies and stability analysis of small-scale unmanned helicopters. (Doctoral Dissertation). University of Manchester. Retrieved from https://www.research.manchester.ac.uk/portal/en/theses/control-strategies-and-stability-analysisof-smallscale-unmanned-helicopters(8e4f8464-6fdd-42e2-9362-033a57a128b2).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.728258

Chicago Manual of Style (16th Edition):

Zhang, Lin. “Control strategies and stability analysis of small-scale unmanned helicopters.” 2017. Doctoral Dissertation, University of Manchester. Accessed April 21, 2021. https://www.research.manchester.ac.uk/portal/en/theses/control-strategies-and-stability-analysisof-smallscale-unmanned-helicopters(8e4f8464-6fdd-42e2-9362-033a57a128b2).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.728258.

MLA Handbook (7th Edition):

Zhang, Lin. “Control strategies and stability analysis of small-scale unmanned helicopters.” 2017. Web. 21 Apr 2021.

Vancouver:

Zhang L. Control strategies and stability analysis of small-scale unmanned helicopters. [Internet] [Doctoral dissertation]. University of Manchester; 2017. [cited 2021 Apr 21]. Available from: https://www.research.manchester.ac.uk/portal/en/theses/control-strategies-and-stability-analysisof-smallscale-unmanned-helicopters(8e4f8464-6fdd-42e2-9362-033a57a128b2).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.728258.

Council of Science Editors:

Zhang L. Control strategies and stability analysis of small-scale unmanned helicopters. [Doctoral Dissertation]. University of Manchester; 2017. Available from: https://www.research.manchester.ac.uk/portal/en/theses/control-strategies-and-stability-analysisof-smallscale-unmanned-helicopters(8e4f8464-6fdd-42e2-9362-033a57a128b2).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.728258

9. Barron, James Richard. Improving finite element methods for fabricated structures.

Degree: PhD, 2000, Imperial College London

Subjects/Keywords: 629.133; Helicopter

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APA (6th Edition):

Barron, J. R. (2000). Improving finite element methods for fabricated structures. (Doctoral Dissertation). Imperial College London. Retrieved from http://hdl.handle.net/10044/1/8022

Chicago Manual of Style (16th Edition):

Barron, James Richard. “Improving finite element methods for fabricated structures.” 2000. Doctoral Dissertation, Imperial College London. Accessed April 21, 2021. http://hdl.handle.net/10044/1/8022.

MLA Handbook (7th Edition):

Barron, James Richard. “Improving finite element methods for fabricated structures.” 2000. Web. 21 Apr 2021.

Vancouver:

Barron JR. Improving finite element methods for fabricated structures. [Internet] [Doctoral dissertation]. Imperial College London; 2000. [cited 2021 Apr 21]. Available from: http://hdl.handle.net/10044/1/8022.

Council of Science Editors:

Barron JR. Improving finite element methods for fabricated structures. [Doctoral Dissertation]. Imperial College London; 2000. Available from: http://hdl.handle.net/10044/1/8022


Delft University of Technology

10. König, Simon (author). Free Water in Helicopter Fuel Tanks: A Computational Prediction Study.

Degree: 2019, Delft University of Technology

Water accumulating in the fuel tanks of any aircraft presents an unacceptable safety hazard. This accumulation, which is due to a combination of physical phenomena,… (more)

Subjects/Keywords: Water; Fuel Tank; Helicopter; Model

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APA (6th Edition):

König, S. (. (2019). Free Water in Helicopter Fuel Tanks: A Computational Prediction Study. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:203dd6ca-d329-4e6e-8e24-0138d83ee869

Chicago Manual of Style (16th Edition):

König, Simon (author). “Free Water in Helicopter Fuel Tanks: A Computational Prediction Study.” 2019. Masters Thesis, Delft University of Technology. Accessed April 21, 2021. http://resolver.tudelft.nl/uuid:203dd6ca-d329-4e6e-8e24-0138d83ee869.

MLA Handbook (7th Edition):

König, Simon (author). “Free Water in Helicopter Fuel Tanks: A Computational Prediction Study.” 2019. Web. 21 Apr 2021.

Vancouver:

König S(. Free Water in Helicopter Fuel Tanks: A Computational Prediction Study. [Internet] [Masters thesis]. Delft University of Technology; 2019. [cited 2021 Apr 21]. Available from: http://resolver.tudelft.nl/uuid:203dd6ca-d329-4e6e-8e24-0138d83ee869.

Council of Science Editors:

König S(. Free Water in Helicopter Fuel Tanks: A Computational Prediction Study. [Masters Thesis]. Delft University of Technology; 2019. Available from: http://resolver.tudelft.nl/uuid:203dd6ca-d329-4e6e-8e24-0138d83ee869


Delft University of Technology

11. Slinger, B.J.M.M. (author). Attitude Control of a Small Helicopter UAV using Incremental Nonlinear Dynamic Inversion.

Degree: 2016, Delft University of Technology

This paper presents an attitude controller for a small helicopter Unmanned Aerial Vehicle (UAV) based on Incremental Nonlinear Dynamic Inversion (INDI). INDI is a sensor-based… (more)

Subjects/Keywords: INDI helicopter uav control attitude

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APA (6th Edition):

Slinger, B. J. M. M. (. (2016). Attitude Control of a Small Helicopter UAV using Incremental Nonlinear Dynamic Inversion. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:9eba1543-6f55-4708-9d68-09446a95d6d4

Chicago Manual of Style (16th Edition):

Slinger, B J M M (author). “Attitude Control of a Small Helicopter UAV using Incremental Nonlinear Dynamic Inversion.” 2016. Masters Thesis, Delft University of Technology. Accessed April 21, 2021. http://resolver.tudelft.nl/uuid:9eba1543-6f55-4708-9d68-09446a95d6d4.

MLA Handbook (7th Edition):

Slinger, B J M M (author). “Attitude Control of a Small Helicopter UAV using Incremental Nonlinear Dynamic Inversion.” 2016. Web. 21 Apr 2021.

Vancouver:

Slinger BJMM(. Attitude Control of a Small Helicopter UAV using Incremental Nonlinear Dynamic Inversion. [Internet] [Masters thesis]. Delft University of Technology; 2016. [cited 2021 Apr 21]. Available from: http://resolver.tudelft.nl/uuid:9eba1543-6f55-4708-9d68-09446a95d6d4.

Council of Science Editors:

Slinger BJMM(. Attitude Control of a Small Helicopter UAV using Incremental Nonlinear Dynamic Inversion. [Masters Thesis]. Delft University of Technology; 2016. Available from: http://resolver.tudelft.nl/uuid:9eba1543-6f55-4708-9d68-09446a95d6d4


Delft University of Technology

12. Blokland, Auke (author). Locating potential landing zones with the help of digital surface models.

Degree: 2018, Delft University of Technology

 The current procedure of the 11 Air Manoeuvre Brigade (11 AMB) is based on a manual non integrated and slow method that uses only outdated… (more)

Subjects/Keywords: DSM; Drone; Helicopter; Military; Satellite

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APA (6th Edition):

Blokland, A. (. (2018). Locating potential landing zones with the help of digital surface models. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:3a923f70-dd0e-4211-9826-7464960ffe3a

Chicago Manual of Style (16th Edition):

Blokland, Auke (author). “Locating potential landing zones with the help of digital surface models.” 2018. Masters Thesis, Delft University of Technology. Accessed April 21, 2021. http://resolver.tudelft.nl/uuid:3a923f70-dd0e-4211-9826-7464960ffe3a.

MLA Handbook (7th Edition):

Blokland, Auke (author). “Locating potential landing zones with the help of digital surface models.” 2018. Web. 21 Apr 2021.

Vancouver:

Blokland A(. Locating potential landing zones with the help of digital surface models. [Internet] [Masters thesis]. Delft University of Technology; 2018. [cited 2021 Apr 21]. Available from: http://resolver.tudelft.nl/uuid:3a923f70-dd0e-4211-9826-7464960ffe3a.

Council of Science Editors:

Blokland A(. Locating potential landing zones with the help of digital surface models. [Masters Thesis]. Delft University of Technology; 2018. Available from: http://resolver.tudelft.nl/uuid:3a923f70-dd0e-4211-9826-7464960ffe3a


Virginia Tech

13. Hatfield, Lauren Michelle. A Qualitative Investigation of Undergraduate Students' Experiences of Helicopter Parenting.

Degree: PhD, Educational Research and Evaluation, 2020, Virginia Tech

 The study involves a qualitative, interview-based investigation of undergraduate students' experiences of helicopter parenting. Little qualitative research, however, has been conducted on the helicopter parenting… (more)

Subjects/Keywords: helicopter parenting; undergraduate students

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APA (6th Edition):

Hatfield, L. M. (2020). A Qualitative Investigation of Undergraduate Students' Experiences of Helicopter Parenting. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/97933

Chicago Manual of Style (16th Edition):

Hatfield, Lauren Michelle. “A Qualitative Investigation of Undergraduate Students' Experiences of Helicopter Parenting.” 2020. Doctoral Dissertation, Virginia Tech. Accessed April 21, 2021. http://hdl.handle.net/10919/97933.

MLA Handbook (7th Edition):

Hatfield, Lauren Michelle. “A Qualitative Investigation of Undergraduate Students' Experiences of Helicopter Parenting.” 2020. Web. 21 Apr 2021.

Vancouver:

Hatfield LM. A Qualitative Investigation of Undergraduate Students' Experiences of Helicopter Parenting. [Internet] [Doctoral dissertation]. Virginia Tech; 2020. [cited 2021 Apr 21]. Available from: http://hdl.handle.net/10919/97933.

Council of Science Editors:

Hatfield LM. A Qualitative Investigation of Undergraduate Students' Experiences of Helicopter Parenting. [Doctoral Dissertation]. Virginia Tech; 2020. Available from: http://hdl.handle.net/10919/97933


University of Toronto

14. Haycock, Bruce Charles. Improved Real-time Helicopter Flight Dynamics Modelling.

Degree: PhD, 2015, University of Toronto

 The University of Toronto Institute for Aerospace Studies has a number of previously developed real-time helicopter models for piloted simulations. An area of concern with… (more)

Subjects/Keywords: Dynamics; Helicopter; Modelling; Simulation; 0538

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APA (6th Edition):

Haycock, B. C. (2015). Improved Real-time Helicopter Flight Dynamics Modelling. (Doctoral Dissertation). University of Toronto. Retrieved from http://hdl.handle.net/1807/70791

Chicago Manual of Style (16th Edition):

Haycock, Bruce Charles. “Improved Real-time Helicopter Flight Dynamics Modelling.” 2015. Doctoral Dissertation, University of Toronto. Accessed April 21, 2021. http://hdl.handle.net/1807/70791.

MLA Handbook (7th Edition):

Haycock, Bruce Charles. “Improved Real-time Helicopter Flight Dynamics Modelling.” 2015. Web. 21 Apr 2021.

Vancouver:

Haycock BC. Improved Real-time Helicopter Flight Dynamics Modelling. [Internet] [Doctoral dissertation]. University of Toronto; 2015. [cited 2021 Apr 21]. Available from: http://hdl.handle.net/1807/70791.

Council of Science Editors:

Haycock BC. Improved Real-time Helicopter Flight Dynamics Modelling. [Doctoral Dissertation]. University of Toronto; 2015. Available from: http://hdl.handle.net/1807/70791


University of Maryland

15. Milluzzo, Joseph. Contributions Towards the Detailed Understanding of Rotor Flow Fields in Ground Effect Operations.

Degree: Aerospace Engineering, 2014, University of Maryland

 High-speed flow visualization and high-resolution particle image velocimetry experiments were conducted on a two-bladed rotor that was operated in a hovering state, both out of… (more)

Subjects/Keywords: Aerospace engineering; Brownout; Helicopter; Rotorcraft

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APA (6th Edition):

Milluzzo, J. (2014). Contributions Towards the Detailed Understanding of Rotor Flow Fields in Ground Effect Operations. (Thesis). University of Maryland. Retrieved from http://hdl.handle.net/1903/15907

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):

Milluzzo, Joseph. “Contributions Towards the Detailed Understanding of Rotor Flow Fields in Ground Effect Operations.” 2014. Thesis, University of Maryland. Accessed April 21, 2021. http://hdl.handle.net/1903/15907.

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

MLA Handbook (7th Edition):

Milluzzo, Joseph. “Contributions Towards the Detailed Understanding of Rotor Flow Fields in Ground Effect Operations.” 2014. Web. 21 Apr 2021.

Vancouver:

Milluzzo J. Contributions Towards the Detailed Understanding of Rotor Flow Fields in Ground Effect Operations. [Internet] [Thesis]. University of Maryland; 2014. [cited 2021 Apr 21]. Available from: http://hdl.handle.net/1903/15907.

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

Council of Science Editors:

Milluzzo J. Contributions Towards the Detailed Understanding of Rotor Flow Fields in Ground Effect Operations. [Thesis]. University of Maryland; 2014. Available from: http://hdl.handle.net/1903/15907

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


Virginia Tech

16. Greer, William Bryce. Advanced Linear Model Predictive Control For Helicopter Shipboard Maneuvers.

Degree: PhD, Aerospace Engineering, 2019, Virginia Tech

 This dissertation proposes and, using simulation, analyzes control algorithms and their use on helicopter shipboard operations. Various benefits and advances for controls in this area… (more)

Subjects/Keywords: Helicopter; Landing; MPC; Control

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APA (6th Edition):

Greer, W. B. (2019). Advanced Linear Model Predictive Control For Helicopter Shipboard Maneuvers. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/95031

Chicago Manual of Style (16th Edition):

Greer, William Bryce. “Advanced Linear Model Predictive Control For Helicopter Shipboard Maneuvers.” 2019. Doctoral Dissertation, Virginia Tech. Accessed April 21, 2021. http://hdl.handle.net/10919/95031.

MLA Handbook (7th Edition):

Greer, William Bryce. “Advanced Linear Model Predictive Control For Helicopter Shipboard Maneuvers.” 2019. Web. 21 Apr 2021.

Vancouver:

Greer WB. Advanced Linear Model Predictive Control For Helicopter Shipboard Maneuvers. [Internet] [Doctoral dissertation]. Virginia Tech; 2019. [cited 2021 Apr 21]. Available from: http://hdl.handle.net/10919/95031.

Council of Science Editors:

Greer WB. Advanced Linear Model Predictive Control For Helicopter Shipboard Maneuvers. [Doctoral Dissertation]. Virginia Tech; 2019. Available from: http://hdl.handle.net/10919/95031


University of Manchester

17. Zhang, Lin. Control strategies and stability analysisof small-scale unmanned helicopters.

Degree: 2017, University of Manchester

 This thesis presents the design and the stability analysis of a hierarchical controller forunmanned aerial vehicles. We utilize non-linear control methodology to command dynamics of… (more)

Subjects/Keywords: helicopter; two-time scale

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APA (6th Edition):

Zhang, L. (2017). Control strategies and stability analysisof small-scale unmanned helicopters. (Doctoral Dissertation). University of Manchester. Retrieved from http://www.manchester.ac.uk/escholar/uk-ac-man-scw:307002

Chicago Manual of Style (16th Edition):

Zhang, Lin. “Control strategies and stability analysisof small-scale unmanned helicopters.” 2017. Doctoral Dissertation, University of Manchester. Accessed April 21, 2021. http://www.manchester.ac.uk/escholar/uk-ac-man-scw:307002.

MLA Handbook (7th Edition):

Zhang, Lin. “Control strategies and stability analysisof small-scale unmanned helicopters.” 2017. Web. 21 Apr 2021.

Vancouver:

Zhang L. Control strategies and stability analysisof small-scale unmanned helicopters. [Internet] [Doctoral dissertation]. University of Manchester; 2017. [cited 2021 Apr 21]. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:307002.

Council of Science Editors:

Zhang L. Control strategies and stability analysisof small-scale unmanned helicopters. [Doctoral Dissertation]. University of Manchester; 2017. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:307002


Delft University of Technology

18. Pardi, Alessandro (author). Improving Helicopter Simulator Fidelity with Augmented Reality: Development and Testing of a Modified Flight Research Simulator where Virtual Windows are made visible through AR Goggles.

Degree: 2020, Delft University of Technology

This project investigates the use of Augmented Reality (AR) in the context of research flight simulators to increase their visual fidelity in rotary-wing applications. The… (more)

Subjects/Keywords: Augmented Reality; helicopter; simulation

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APA (6th Edition):

Pardi, A. (. (2020). Improving Helicopter Simulator Fidelity with Augmented Reality: Development and Testing of a Modified Flight Research Simulator where Virtual Windows are made visible through AR Goggles. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:9e60139b-6f3b-49e2-a5b5-7c1ecf30ad25

Chicago Manual of Style (16th Edition):

Pardi, Alessandro (author). “Improving Helicopter Simulator Fidelity with Augmented Reality: Development and Testing of a Modified Flight Research Simulator where Virtual Windows are made visible through AR Goggles.” 2020. Masters Thesis, Delft University of Technology. Accessed April 21, 2021. http://resolver.tudelft.nl/uuid:9e60139b-6f3b-49e2-a5b5-7c1ecf30ad25.

MLA Handbook (7th Edition):

Pardi, Alessandro (author). “Improving Helicopter Simulator Fidelity with Augmented Reality: Development and Testing of a Modified Flight Research Simulator where Virtual Windows are made visible through AR Goggles.” 2020. Web. 21 Apr 2021.

Vancouver:

Pardi A(. Improving Helicopter Simulator Fidelity with Augmented Reality: Development and Testing of a Modified Flight Research Simulator where Virtual Windows are made visible through AR Goggles. [Internet] [Masters thesis]. Delft University of Technology; 2020. [cited 2021 Apr 21]. Available from: http://resolver.tudelft.nl/uuid:9e60139b-6f3b-49e2-a5b5-7c1ecf30ad25.

Council of Science Editors:

Pardi A(. Improving Helicopter Simulator Fidelity with Augmented Reality: Development and Testing of a Modified Flight Research Simulator where Virtual Windows are made visible through AR Goggles. [Masters Thesis]. Delft University of Technology; 2020. Available from: http://resolver.tudelft.nl/uuid:9e60139b-6f3b-49e2-a5b5-7c1ecf30ad25


University of Texas – Austin

19. Karpatne, Anand. Study of compressible flow through a rotating duct.

Degree: PhD, Aerospace engineering, 2015, University of Texas – Austin

 Several rotorcraft applications such as circulation control and tip jet driven rotors involve internal spanwise flow along the interior of a rotor blade. This dissertation… (more)

Subjects/Keywords: Helicopter; Rotor; Internal flow

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

APA (6th Edition):

Karpatne, A. (2015). Study of compressible flow through a rotating duct. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/31343

Chicago Manual of Style (16th Edition):

Karpatne, Anand. “Study of compressible flow through a rotating duct.” 2015. Doctoral Dissertation, University of Texas – Austin. Accessed April 21, 2021. http://hdl.handle.net/2152/31343.

MLA Handbook (7th Edition):

Karpatne, Anand. “Study of compressible flow through a rotating duct.” 2015. Web. 21 Apr 2021.

Vancouver:

Karpatne A. Study of compressible flow through a rotating duct. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2015. [cited 2021 Apr 21]. Available from: http://hdl.handle.net/2152/31343.

Council of Science Editors:

Karpatne A. Study of compressible flow through a rotating duct. [Doctoral Dissertation]. University of Texas – Austin; 2015. Available from: http://hdl.handle.net/2152/31343


Penn State University

20. Metkowski, Leonard P. Experimental study of wake impingement on a horizontal stabalizer.

Degree: 2018, Penn State University

 The design and execution of a full-scale Reynold’s number water tunnel experiment was performed to create a data set used to analyze the effects of… (more)

Subjects/Keywords: Aerodynamics; Helicopter; Hubs; Empennage; Experimental; Interactional Aerodynamics; Helicopter Hub Drag; Experimental Design; Helicopter Hub Experiments; Horizontal Stabilizer; Helicopter Stabilizer; Experiments on Helicopter Stabilizers; Wake Impingement

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APA (6th Edition):

Metkowski, L. P. (2018). Experimental study of wake impingement on a horizontal stabalizer. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/14712lpm5054

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):

Metkowski, Leonard P. “Experimental study of wake impingement on a horizontal stabalizer.” 2018. Thesis, Penn State University. Accessed April 21, 2021. https://submit-etda.libraries.psu.edu/catalog/14712lpm5054.

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

MLA Handbook (7th Edition):

Metkowski, Leonard P. “Experimental study of wake impingement on a horizontal stabalizer.” 2018. Web. 21 Apr 2021.

Vancouver:

Metkowski LP. Experimental study of wake impingement on a horizontal stabalizer. [Internet] [Thesis]. Penn State University; 2018. [cited 2021 Apr 21]. Available from: https://submit-etda.libraries.psu.edu/catalog/14712lpm5054.

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

Council of Science Editors:

Metkowski LP. Experimental study of wake impingement on a horizontal stabalizer. [Thesis]. Penn State University; 2018. Available from: https://submit-etda.libraries.psu.edu/catalog/14712lpm5054

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


Cornell University

21. Fang, Austin. Improved Rotor Track And Balance Algorithm And System Identification Of Rotorcraft Using Flight Data.

Degree: PhD, Aerospace Engineering, 2015, Cornell University

 Rotor track and balance is an essential part of maintenance for the rotorcraft industry. Methods for solving rotor track and balance problems to minimize undesirable… (more)

Subjects/Keywords: Rotor Track and Balance; Rotorcraft; Helicopter Tuning

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APA (6th Edition):

Fang, A. (2015). Improved Rotor Track And Balance Algorithm And System Identification Of Rotorcraft Using Flight Data. (Doctoral Dissertation). Cornell University. Retrieved from http://hdl.handle.net/1813/39294

Chicago Manual of Style (16th Edition):

Fang, Austin. “Improved Rotor Track And Balance Algorithm And System Identification Of Rotorcraft Using Flight Data.” 2015. Doctoral Dissertation, Cornell University. Accessed April 21, 2021. http://hdl.handle.net/1813/39294.

MLA Handbook (7th Edition):

Fang, Austin. “Improved Rotor Track And Balance Algorithm And System Identification Of Rotorcraft Using Flight Data.” 2015. Web. 21 Apr 2021.

Vancouver:

Fang A. Improved Rotor Track And Balance Algorithm And System Identification Of Rotorcraft Using Flight Data. [Internet] [Doctoral dissertation]. Cornell University; 2015. [cited 2021 Apr 21]. Available from: http://hdl.handle.net/1813/39294.

Council of Science Editors:

Fang A. Improved Rotor Track And Balance Algorithm And System Identification Of Rotorcraft Using Flight Data. [Doctoral Dissertation]. Cornell University; 2015. Available from: http://hdl.handle.net/1813/39294


Texas A&M University

22. Sunberg, Zachary Nolan. A Real Time Expert Control System for Helicopter Autorotation.

Degree: MS, Aerospace Engineering, 2013, Texas A&M University

 Autorotation maneuvers are required to perform a safe landing of a helicopter in cases of engine loss in a single engine vehicle and transmission or… (more)

Subjects/Keywords: Autorotation; Expert System; Fuzzy Logic; Control; Helicopter

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APA (6th Edition):

Sunberg, Z. N. (2013). A Real Time Expert Control System for Helicopter Autorotation. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/149553

Chicago Manual of Style (16th Edition):

Sunberg, Zachary Nolan. “A Real Time Expert Control System for Helicopter Autorotation.” 2013. Masters Thesis, Texas A&M University. Accessed April 21, 2021. http://hdl.handle.net/1969.1/149553.

MLA Handbook (7th Edition):

Sunberg, Zachary Nolan. “A Real Time Expert Control System for Helicopter Autorotation.” 2013. Web. 21 Apr 2021.

Vancouver:

Sunberg ZN. A Real Time Expert Control System for Helicopter Autorotation. [Internet] [Masters thesis]. Texas A&M University; 2013. [cited 2021 Apr 21]. Available from: http://hdl.handle.net/1969.1/149553.

Council of Science Editors:

Sunberg ZN. A Real Time Expert Control System for Helicopter Autorotation. [Masters Thesis]. Texas A&M University; 2013. Available from: http://hdl.handle.net/1969.1/149553


Penn State University

23. Caudle, David Burdette. Damage Mitigation for Rotorcraft through Load Alleviating Control.

Degree: 2014, Penn State University

 A control method was developed to reduce the fatigue damage caused to critical rotorcraft hub components. This control method was demonstrated using simulation models of… (more)

Subjects/Keywords: rotorcraft; helicopter; damage mitigation; control; load alleviation

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APA (6th Edition):

Caudle, D. B. (2014). Damage Mitigation for Rotorcraft through Load Alleviating Control. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/23708

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):

Caudle, David Burdette. “Damage Mitigation for Rotorcraft through Load Alleviating Control.” 2014. Thesis, Penn State University. Accessed April 21, 2021. https://submit-etda.libraries.psu.edu/catalog/23708.

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

MLA Handbook (7th Edition):

Caudle, David Burdette. “Damage Mitigation for Rotorcraft through Load Alleviating Control.” 2014. Web. 21 Apr 2021.

Vancouver:

Caudle DB. Damage Mitigation for Rotorcraft through Load Alleviating Control. [Internet] [Thesis]. Penn State University; 2014. [cited 2021 Apr 21]. Available from: https://submit-etda.libraries.psu.edu/catalog/23708.

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

Council of Science Editors:

Caudle DB. Damage Mitigation for Rotorcraft through Load Alleviating Control. [Thesis]. Penn State University; 2014. Available from: https://submit-etda.libraries.psu.edu/catalog/23708

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


Penn State University

24. Schafer, Sylvie Ann. Flight Test Measurement of Ship Airwake Disturbances Using Small-scale Rotorcraft.

Degree: 2015, Penn State University

 The maritime environment is one of the most challenging operating environments for helicopters. The vertical takeoff and landing capability that helicopters possess make then uniquely… (more)

Subjects/Keywords: flight test; airwake; helicopter; gust identification

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APA (6th Edition):

Schafer, S. A. (2015). Flight Test Measurement of Ship Airwake Disturbances Using Small-scale Rotorcraft. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/26608

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):

Schafer, Sylvie Ann. “Flight Test Measurement of Ship Airwake Disturbances Using Small-scale Rotorcraft.” 2015. Thesis, Penn State University. Accessed April 21, 2021. https://submit-etda.libraries.psu.edu/catalog/26608.

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

MLA Handbook (7th Edition):

Schafer, Sylvie Ann. “Flight Test Measurement of Ship Airwake Disturbances Using Small-scale Rotorcraft.” 2015. Web. 21 Apr 2021.

Vancouver:

Schafer SA. Flight Test Measurement of Ship Airwake Disturbances Using Small-scale Rotorcraft. [Internet] [Thesis]. Penn State University; 2015. [cited 2021 Apr 21]. Available from: https://submit-etda.libraries.psu.edu/catalog/26608.

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

Council of Science Editors:

Schafer SA. Flight Test Measurement of Ship Airwake Disturbances Using Small-scale Rotorcraft. [Thesis]. Penn State University; 2015. Available from: https://submit-etda.libraries.psu.edu/catalog/26608

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


Penn State University

25. Villafana, Willca. Rotorcraft Noise Abatement Procedures Development.

Degree: 2016, Penn State University

 A rotorcraft noise prediction system has recently been developed as part of a project to develop and evaluate helicopter noise abatement procedures for a range… (more)

Subjects/Keywords: aeroacoustics; helicopter; rotor noise; simulation; modeling

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APA (6th Edition):

Villafana, W. (2016). Rotorcraft Noise Abatement Procedures Development. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/13106wrv105

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):

Villafana, Willca. “Rotorcraft Noise Abatement Procedures Development.” 2016. Thesis, Penn State University. Accessed April 21, 2021. https://submit-etda.libraries.psu.edu/catalog/13106wrv105.

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

MLA Handbook (7th Edition):

Villafana, Willca. “Rotorcraft Noise Abatement Procedures Development.” 2016. Web. 21 Apr 2021.

Vancouver:

Villafana W. Rotorcraft Noise Abatement Procedures Development. [Internet] [Thesis]. Penn State University; 2016. [cited 2021 Apr 21]. Available from: https://submit-etda.libraries.psu.edu/catalog/13106wrv105.

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

Council of Science Editors:

Villafana W. Rotorcraft Noise Abatement Procedures Development. [Thesis]. Penn State University; 2016. Available from: https://submit-etda.libraries.psu.edu/catalog/13106wrv105

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


Penn State University

26. Malovrh, Brendon. Non-harmonic Root-pitch Individual-blade Control for the Reduction of Blade-vortex Interaction Noise in Rotorcraft.

Degree: 2012, Penn State University

 One of the greatest obstacles to public acceptance of rotorcraft is the high levels of noise they produce, particularly in low-speed descent. In this flight… (more)

Subjects/Keywords: Blade-Vortex Interaction; BVI; noise; acoustic; helicopter

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APA (6th Edition):

Malovrh, B. (2012). Non-harmonic Root-pitch Individual-blade Control for the Reduction of Blade-vortex Interaction Noise in Rotorcraft. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/15596

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):

Malovrh, Brendon. “Non-harmonic Root-pitch Individual-blade Control for the Reduction of Blade-vortex Interaction Noise in Rotorcraft.” 2012. Thesis, Penn State University. Accessed April 21, 2021. https://submit-etda.libraries.psu.edu/catalog/15596.

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

MLA Handbook (7th Edition):

Malovrh, Brendon. “Non-harmonic Root-pitch Individual-blade Control for the Reduction of Blade-vortex Interaction Noise in Rotorcraft.” 2012. Web. 21 Apr 2021.

Vancouver:

Malovrh B. Non-harmonic Root-pitch Individual-blade Control for the Reduction of Blade-vortex Interaction Noise in Rotorcraft. [Internet] [Thesis]. Penn State University; 2012. [cited 2021 Apr 21]. Available from: https://submit-etda.libraries.psu.edu/catalog/15596.

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

Council of Science Editors:

Malovrh B. Non-harmonic Root-pitch Individual-blade Control for the Reduction of Blade-vortex Interaction Noise in Rotorcraft. [Thesis]. Penn State University; 2012. Available from: https://submit-etda.libraries.psu.edu/catalog/15596

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


Penn State University

27. Han, Yiqiang. THEORETICAL AND EXPERIMENTAL STUDY OF SCALING METHOD IN THE ROTOR BLADE ICE ACCRETION TEST .

Degree: 2011, Penn State University

 In the ice accretion test, due to the limitation of test section size and icing condition capability of the test facility, an icing test on… (more)

Subjects/Keywords: Helicopter Icing; Scaling Method; Ice Accretion Test

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APA (6th Edition):

Han, Y. (2011). THEORETICAL AND EXPERIMENTAL STUDY OF SCALING METHOD IN THE ROTOR BLADE ICE ACCRETION TEST . (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/11937

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):

Han, Yiqiang. “THEORETICAL AND EXPERIMENTAL STUDY OF SCALING METHOD IN THE ROTOR BLADE ICE ACCRETION TEST .” 2011. Thesis, Penn State University. Accessed April 21, 2021. https://submit-etda.libraries.psu.edu/catalog/11937.

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

MLA Handbook (7th Edition):

Han, Yiqiang. “THEORETICAL AND EXPERIMENTAL STUDY OF SCALING METHOD IN THE ROTOR BLADE ICE ACCRETION TEST .” 2011. Web. 21 Apr 2021.

Vancouver:

Han Y. THEORETICAL AND EXPERIMENTAL STUDY OF SCALING METHOD IN THE ROTOR BLADE ICE ACCRETION TEST . [Internet] [Thesis]. Penn State University; 2011. [cited 2021 Apr 21]. Available from: https://submit-etda.libraries.psu.edu/catalog/11937.

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

Council of Science Editors:

Han Y. THEORETICAL AND EXPERIMENTAL STUDY OF SCALING METHOD IN THE ROTOR BLADE ICE ACCRETION TEST . [Thesis]. Penn State University; 2011. Available from: https://submit-etda.libraries.psu.edu/catalog/11937

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


Indian Institute of Science

28. Chandra Sekhar, D. Efficient Trim In Helicopter Aeroelastic Analysis.

Degree: MSc Engg, Faculty of Engineering, 2011, Indian Institute of Science

Helicopter aeroelastic analysis is highly complex and multidisciplinary in nature; the flexibility of main rotor blades is coupled with aerodynamics, dynamics and control systems. A… (more)

Subjects/Keywords: Helicopter - Aeroelasticity; Helicopter Rotor Blades; Helicopters - Aerolastic Analysis; Rotocraft Trim; Helicopters - Trim Analysis; Rotors (Helicopters); Helicopter Trim - Numerical Analysis; Rotors - Aeroelastic Optimization; Aeroelastic Analysis; Helicopter Trim; Aeronautics

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APA (6th Edition):

Chandra Sekhar, D. (2011). Efficient Trim In Helicopter Aeroelastic Analysis. (Masters Thesis). Indian Institute of Science. Retrieved from http://etd.iisc.ac.in/handle/2005/1118

Chicago Manual of Style (16th Edition):

Chandra Sekhar, D. “Efficient Trim In Helicopter Aeroelastic Analysis.” 2011. Masters Thesis, Indian Institute of Science. Accessed April 21, 2021. http://etd.iisc.ac.in/handle/2005/1118.

MLA Handbook (7th Edition):

Chandra Sekhar, D. “Efficient Trim In Helicopter Aeroelastic Analysis.” 2011. Web. 21 Apr 2021.

Vancouver:

Chandra Sekhar D. Efficient Trim In Helicopter Aeroelastic Analysis. [Internet] [Masters thesis]. Indian Institute of Science; 2011. [cited 2021 Apr 21]. Available from: http://etd.iisc.ac.in/handle/2005/1118.

Council of Science Editors:

Chandra Sekhar D. Efficient Trim In Helicopter Aeroelastic Analysis. [Masters Thesis]. Indian Institute of Science; 2011. Available from: http://etd.iisc.ac.in/handle/2005/1118


Queensland University of Technology

29. Locke, Judith Y. Too much of a good thing?: An investigation into overparenting.

Degree: 2014, Queensland University of Technology

 This project investigated the concept of overparenting, parenting which over uses valued parenting practices, such as protection and care for offspring. It established a clearer… (more)

Subjects/Keywords: overparenting; helicopter parenting; children; adolescents; measures; homework

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APA (6th Edition):

Locke, J. Y. (2014). Too much of a good thing?: An investigation into overparenting. (Thesis). Queensland University of Technology. Retrieved from https://eprints.qut.edu.au/72871/

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):

Locke, Judith Y. “Too much of a good thing?: An investigation into overparenting.” 2014. Thesis, Queensland University of Technology. Accessed April 21, 2021. https://eprints.qut.edu.au/72871/.

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

MLA Handbook (7th Edition):

Locke, Judith Y. “Too much of a good thing?: An investigation into overparenting.” 2014. Web. 21 Apr 2021.

Vancouver:

Locke JY. Too much of a good thing?: An investigation into overparenting. [Internet] [Thesis]. Queensland University of Technology; 2014. [cited 2021 Apr 21]. Available from: https://eprints.qut.edu.au/72871/.

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

Council of Science Editors:

Locke JY. Too much of a good thing?: An investigation into overparenting. [Thesis]. Queensland University of Technology; 2014. Available from: https://eprints.qut.edu.au/72871/

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


RMIT University

30. Johnston, V. Design, manufacture and testing of a multi-platform Mach scale composite rotor blade.

Degree: 2011, RMIT University

 The scope of this study includes the design, manufacture and experimental hover testing of baseline and improved Mach scale composite blades to prove the performance… (more)

Subjects/Keywords: Fields of Research; Composites; aerospace; helicopter blades

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

APA (6th Edition):

Johnston, V. (2011). Design, manufacture and testing of a multi-platform Mach scale composite rotor blade. (Thesis). RMIT University. Retrieved from http://researchbank.rmit.edu.au/view/rmit:160965

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):

Johnston, V. “Design, manufacture and testing of a multi-platform Mach scale composite rotor blade.” 2011. Thesis, RMIT University. Accessed April 21, 2021. http://researchbank.rmit.edu.au/view/rmit:160965.

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

MLA Handbook (7th Edition):

Johnston, V. “Design, manufacture and testing of a multi-platform Mach scale composite rotor blade.” 2011. Web. 21 Apr 2021.

Vancouver:

Johnston V. Design, manufacture and testing of a multi-platform Mach scale composite rotor blade. [Internet] [Thesis]. RMIT University; 2011. [cited 2021 Apr 21]. Available from: http://researchbank.rmit.edu.au/view/rmit:160965.

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

Council of Science Editors:

Johnston V. Design, manufacture and testing of a multi-platform Mach scale composite rotor blade. [Thesis]. RMIT University; 2011. Available from: http://researchbank.rmit.edu.au/view/rmit:160965

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

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