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You searched for subject:(Helicopter). Showing records 1 – 30 of 335 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: MS, Aerospace Engineering, 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 · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Walsh, Gregory Daniel. “A PRELIMINARY ACOUSTIC INVESTIGATION OF A COAXIAL HELICOPTER IN HIGH-SPEED FLIGHT.” 2016. Masters Thesis, Penn State University. Accessed April 21, 2019. https://etda.libraries.psu.edu/catalog/c534fn92g.

MLA Handbook (7th Edition):

Walsh, Gregory Daniel. “A PRELIMINARY ACOUSTIC INVESTIGATION OF A COAXIAL HELICOPTER IN HIGH-SPEED FLIGHT.” 2016. Web. 21 Apr 2019.

Vancouver:

Walsh GD. A PRELIMINARY ACOUSTIC INVESTIGATION OF A COAXIAL HELICOPTER IN HIGH-SPEED FLIGHT. [Internet] [Masters thesis]. Penn State University; 2016. [cited 2019 Apr 21]. Available from: https://etda.libraries.psu.edu/catalog/c534fn92g.

Council of Science Editors:

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


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, 2019. 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 2019.

Vancouver:

Jia Y. A multi-input multi-output self tuning regulator for nonlinear helicopter control . [Internet] [Thesis]. California State University – Chico; 2013. [cited 2019 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


University of Alberta

3. 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, 2019. 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 2019.

Vancouver:

Godbolt BM. Experimental Nonlinear Control of a Helicopter Unmanned Aerial Vehicle (UAV). [Internet] [Doctoral dissertation]. University of Alberta; 2013. [cited 2019 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


Texas A&M University

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

Degree: 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. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/149488

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):

Taylor, Bradley Whitten. “Experimental Investigation of Helicopter Weight and Mass Center Estimation.” 2013. Thesis, Texas A&M University. Accessed April 21, 2019. http://hdl.handle.net/1969.1/149488.

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

MLA Handbook (7th Edition):

Taylor, Bradley Whitten. “Experimental Investigation of Helicopter Weight and Mass Center Estimation.” 2013. Web. 21 Apr 2019.

Vancouver:

Taylor BW. Experimental Investigation of Helicopter Weight and Mass Center Estimation. [Internet] [Thesis]. Texas A&M University; 2013. [cited 2019 Apr 21]. Available from: http://hdl.handle.net/1969.1/149488.

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

Council of Science Editors:

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

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

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, 2019. 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 2019.

Vancouver:

T S. Modeling and analysis of helicopter vibrations during dynamic conditions;. [Internet] [Thesis]. Kuvempu University; 2014. [cited 2019 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


University of Manchester

6. 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: two-time scale; helicopter

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

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 ; http://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, 2019. https://www.research.manchester.ac.uk/portal/en/theses/control-strategies-and-stability-analysisof-smallscale-unmanned-helicopters(8e4f8464-6fdd-42e2-9362-033a57a128b2).html ; http://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 2019.

Vancouver:

Zhang L. Control strategies and stability analysis of small-scale unmanned helicopters. [Internet] [Doctoral dissertation]. University of Manchester; 2017. [cited 2019 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 ; http://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 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.728258


Penn State University

7. Corl, Jonas Daniel. A COMPARISON OF HELICOPTER ACTIVE ROTOR GUST REJECTION AND VIBRATION ALLEVIATION METHODS.

Degree: MS, Mechanical Engineering, 2009, Penn State University

 Dynamic Interface (DI) tasks such as station keeping, takeoff, and landing during helicopter-ship interactions are often unacceptably workload-intensive due not only to close quarters and… (more)

Subjects/Keywords: helicopter; swashplate; active rotor

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APA (6th Edition):

Corl, J. D. (2009). A COMPARISON OF HELICOPTER ACTIVE ROTOR GUST REJECTION AND VIBRATION ALLEVIATION METHODS. (Masters Thesis). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/9978

Chicago Manual of Style (16th Edition):

Corl, Jonas Daniel. “A COMPARISON OF HELICOPTER ACTIVE ROTOR GUST REJECTION AND VIBRATION ALLEVIATION METHODS.” 2009. Masters Thesis, Penn State University. Accessed April 21, 2019. https://etda.libraries.psu.edu/catalog/9978.

MLA Handbook (7th Edition):

Corl, Jonas Daniel. “A COMPARISON OF HELICOPTER ACTIVE ROTOR GUST REJECTION AND VIBRATION ALLEVIATION METHODS.” 2009. Web. 21 Apr 2019.

Vancouver:

Corl JD. A COMPARISON OF HELICOPTER ACTIVE ROTOR GUST REJECTION AND VIBRATION ALLEVIATION METHODS. [Internet] [Masters thesis]. Penn State University; 2009. [cited 2019 Apr 21]. Available from: https://etda.libraries.psu.edu/catalog/9978.

Council of Science Editors:

Corl JD. A COMPARISON OF HELICOPTER ACTIVE ROTOR GUST REJECTION AND VIBRATION ALLEVIATION METHODS. [Masters Thesis]. Penn State University; 2009. Available from: https://etda.libraries.psu.edu/catalog/9978


University of Manchester

8. 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, 2019. 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 2019.

Vancouver:

Zhang L. Control strategies and stability analysisof small-scale unmanned helicopters. [Internet] [Doctoral dissertation]. University of Manchester; 2017. [cited 2019 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

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, 2019. 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 2019.

Vancouver:

Barron JR. Improving finite element methods for fabricated structures. [Internet] [Doctoral dissertation]. Imperial College London; 2000. [cited 2019 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


University of Toronto

10. 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, 2019. http://hdl.handle.net/1807/70791.

MLA Handbook (7th Edition):

Haycock, Bruce Charles. “Improved Real-time Helicopter Flight Dynamics Modelling.” 2015. Web. 21 Apr 2019.

Vancouver:

Haycock BC. Improved Real-time Helicopter Flight Dynamics Modelling. [Internet] [Doctoral dissertation]. University of Toronto; 2015. [cited 2019 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 Texas – Austin

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

Degree: 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 (6th Edition):

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

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):

Karpatne, Anand. “Study of compressible flow through a rotating duct.” 2015. Thesis, University of Texas – Austin. Accessed April 21, 2019. http://hdl.handle.net/2152/31343.

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

MLA Handbook (7th Edition):

Karpatne, Anand. “Study of compressible flow through a rotating duct.” 2015. Web. 21 Apr 2019.

Vancouver:

Karpatne A. Study of compressible flow through a rotating duct. [Internet] [Thesis]. University of Texas – Austin; 2015. [cited 2019 Apr 21]. Available from: http://hdl.handle.net/2152/31343.

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

Council of Science Editors:

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

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


Penn State University

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

Degree: 2018, Penn State University

 The design and execution of a full-scale Reynolds number water tunnel experiment was performedto create a data set used to analyze the effects of wake… (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. (2018). Experimental study of wake impingement on a horizontal stabalizer. (Thesis). Penn State University. Retrieved from https://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. “Experimental study of wake impingement on a horizontal stabalizer.” 2018. Thesis, Penn State University. Accessed April 21, 2019. https://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. “Experimental study of wake impingement on a horizontal stabalizer.” 2018. Web. 21 Apr 2019.

Vancouver:

Metkowski L. Experimental study of wake impingement on a horizontal stabalizer. [Internet] [Thesis]. Penn State University; 2018. [cited 2019 Apr 21]. Available from: https://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 L. Experimental study of wake impingement on a horizontal stabalizer. [Thesis]. Penn State University; 2018. Available from: https://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


Cranfield University

13. Mostafa, A. A design study for a compound helicopter featured with a convertible prop/rotor.

Degree: PhD, 1989, Cranfield University

 A compound helicopter is a hybrid vehicle, fundamentally a helicopter. It uses an auxiliary lift and propulsion device(s) in order to eliminate the lifting rotor… (more)

Subjects/Keywords: 629.133; Helicopter design

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APA (6th Edition):

Mostafa, A. (1989). A design study for a compound helicopter featured with a convertible prop/rotor. (Doctoral Dissertation). Cranfield University. Retrieved from http://dspace.lib.cranfield.ac.uk/handle/1826/11049 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.253415

Chicago Manual of Style (16th Edition):

Mostafa, A. “A design study for a compound helicopter featured with a convertible prop/rotor.” 1989. Doctoral Dissertation, Cranfield University. Accessed April 21, 2019. http://dspace.lib.cranfield.ac.uk/handle/1826/11049 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.253415.

MLA Handbook (7th Edition):

Mostafa, A. “A design study for a compound helicopter featured with a convertible prop/rotor.” 1989. Web. 21 Apr 2019.

Vancouver:

Mostafa A. A design study for a compound helicopter featured with a convertible prop/rotor. [Internet] [Doctoral dissertation]. Cranfield University; 1989. [cited 2019 Apr 21]. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/11049 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.253415.

Council of Science Editors:

Mostafa A. A design study for a compound helicopter featured with a convertible prop/rotor. [Doctoral Dissertation]. Cranfield University; 1989. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/11049 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.253415


Indian Institute of Science

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

Degree: 2009, 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. (2009). Efficient Trim In Helicopter Aeroelastic Analysis. (Thesis). Indian Institute of Science. Retrieved from http://hdl.handle.net/2005/1118

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):

Chandra Sekhar, D. “Efficient Trim In Helicopter Aeroelastic Analysis.” 2009. Thesis, Indian Institute of Science. Accessed April 21, 2019. http://hdl.handle.net/2005/1118.

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

MLA Handbook (7th Edition):

Chandra Sekhar, D. “Efficient Trim In Helicopter Aeroelastic Analysis.” 2009. Web. 21 Apr 2019.

Vancouver:

Chandra Sekhar D. Efficient Trim In Helicopter Aeroelastic Analysis. [Internet] [Thesis]. Indian Institute of Science; 2009. [cited 2019 Apr 21]. Available from: http://hdl.handle.net/2005/1118.

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

Council of Science Editors:

Chandra Sekhar D. Efficient Trim In Helicopter Aeroelastic Analysis. [Thesis]. Indian Institute of Science; 2009. Available from: http://hdl.handle.net/2005/1118

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


Texas A&M University

15. Ruiz Brito, Luis A. Control of a 3DOF Birotor Helicopter Using Robust Control Methods.

Degree: 2010, Texas A&M University

 The main topic of this thesis is to exhibit how robust control techniques can be applied to real time systems. Presently, the control techniques used… (more)

Subjects/Keywords: birotor helicopter h infinity robust control

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APA (6th Edition):

Ruiz Brito, L. A. (2010). Control of a 3DOF Birotor Helicopter Using Robust Control Methods. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2009-12-7397

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):

Ruiz Brito, Luis A. “Control of a 3DOF Birotor Helicopter Using Robust Control Methods.” 2010. Thesis, Texas A&M University. Accessed April 21, 2019. http://hdl.handle.net/1969.1/ETD-TAMU-2009-12-7397.

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

MLA Handbook (7th Edition):

Ruiz Brito, Luis A. “Control of a 3DOF Birotor Helicopter Using Robust Control Methods.” 2010. Web. 21 Apr 2019.

Vancouver:

Ruiz Brito LA. Control of a 3DOF Birotor Helicopter Using Robust Control Methods. [Internet] [Thesis]. Texas A&M University; 2010. [cited 2019 Apr 21]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2009-12-7397.

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

Council of Science Editors:

Ruiz Brito LA. Control of a 3DOF Birotor Helicopter Using Robust Control Methods. [Thesis]. Texas A&M University; 2010. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2009-12-7397

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


Texas A&M University

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

Degree: 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. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/149553

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):

Sunberg, Zachary Nolan. “A Real Time Expert Control System for Helicopter Autorotation.” 2013. Thesis, Texas A&M University. Accessed April 21, 2019. http://hdl.handle.net/1969.1/149553.

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

MLA Handbook (7th Edition):

Sunberg, Zachary Nolan. “A Real Time Expert Control System for Helicopter Autorotation.” 2013. Web. 21 Apr 2019.

Vancouver:

Sunberg ZN. A Real Time Expert Control System for Helicopter Autorotation. [Internet] [Thesis]. Texas A&M University; 2013. [cited 2019 Apr 21]. Available from: http://hdl.handle.net/1969.1/149553.

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

Council of Science Editors:

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

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


Penn State University

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

Degree: MS, Aerospace Engineering, 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 · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Villafana, Willca. “Rotorcraft Noise Abatement Procedures Development.” 2016. Masters Thesis, Penn State University. Accessed April 21, 2019. https://etda.libraries.psu.edu/catalog/13106wrv105.

MLA Handbook (7th Edition):

Villafana, Willca. “Rotorcraft Noise Abatement Procedures Development.” 2016. Web. 21 Apr 2019.

Vancouver:

Villafana W. Rotorcraft Noise Abatement Procedures Development. [Internet] [Masters thesis]. Penn State University; 2016. [cited 2019 Apr 21]. Available from: https://etda.libraries.psu.edu/catalog/13106wrv105.

Council of Science Editors:

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


Penn State University

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

Degree: MS, Aerospace Engineering, 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 · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Han, Yiqiang. “THEORETICAL AND EXPERIMENTAL STUDY OF SCALING METHOD IN THE ROTOR BLADE ICE ACCRETION TEST.” 2011. Masters Thesis, Penn State University. Accessed April 21, 2019. https://etda.libraries.psu.edu/catalog/11937.

MLA Handbook (7th Edition):

Han, Yiqiang. “THEORETICAL AND EXPERIMENTAL STUDY OF SCALING METHOD IN THE ROTOR BLADE ICE ACCRETION TEST.” 2011. Web. 21 Apr 2019.

Vancouver:

Han Y. THEORETICAL AND EXPERIMENTAL STUDY OF SCALING METHOD IN THE ROTOR BLADE ICE ACCRETION TEST. [Internet] [Masters thesis]. Penn State University; 2011. [cited 2019 Apr 21]. Available from: https://etda.libraries.psu.edu/catalog/11937.

Council of Science Editors:

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


Penn State University

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

Degree: MS, Aerospace Engineering, 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. (Masters Thesis). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/23708

Chicago Manual of Style (16th Edition):

Caudle, David Burdette. “Damage Mitigation for Rotorcraft through Load Alleviating Control.” 2014. Masters Thesis, Penn State University. Accessed April 21, 2019. https://etda.libraries.psu.edu/catalog/23708.

MLA Handbook (7th Edition):

Caudle, David Burdette. “Damage Mitigation for Rotorcraft through Load Alleviating Control.” 2014. Web. 21 Apr 2019.

Vancouver:

Caudle DB. Damage Mitigation for Rotorcraft through Load Alleviating Control. [Internet] [Masters thesis]. Penn State University; 2014. [cited 2019 Apr 21]. Available from: https://etda.libraries.psu.edu/catalog/23708.

Council of Science Editors:

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


Penn State University

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

Degree: PhD, Aerospace Engineering, 2010, 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. (2010). Non-harmonic Root-pitch Individual-blade Control for the Reduction of Blade-vortex Interaction Noise in Rotorcraft. (Doctoral Dissertation). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/15596

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.” 2010. Doctoral Dissertation, Penn State University. Accessed April 21, 2019. https://etda.libraries.psu.edu/catalog/15596.

MLA Handbook (7th Edition):

Malovrh, Brendon. “Non-harmonic Root-pitch Individual-blade Control for the Reduction of Blade-vortex Interaction Noise in Rotorcraft.” 2010. Web. 21 Apr 2019.

Vancouver:

Malovrh B. Non-harmonic Root-pitch Individual-blade Control for the Reduction of Blade-vortex Interaction Noise in Rotorcraft. [Internet] [Doctoral dissertation]. Penn State University; 2010. [cited 2019 Apr 21]. Available from: https://etda.libraries.psu.edu/catalog/15596.

Council of Science Editors:

Malovrh B. Non-harmonic Root-pitch Individual-blade Control for the Reduction of Blade-vortex Interaction Noise in Rotorcraft. [Doctoral Dissertation]. Penn State University; 2010. Available from: https://etda.libraries.psu.edu/catalog/15596


Queensland University of Technology

21. 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, 2019. 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 2019.

Vancouver:

Locke JY. Too much of a good thing?: An investigation into overparenting. [Internet] [Thesis]. Queensland University of Technology; 2014. [cited 2019 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


Cornell University

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

Degree: 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 . (Thesis). Cornell University. Retrieved from http://hdl.handle.net/1813/39294

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):

Fang, Austin. “Improved Rotor Track And Balance Algorithm And System Identification Of Rotorcraft Using Flight Data .” 2015. Thesis, Cornell University. Accessed April 21, 2019. http://hdl.handle.net/1813/39294.

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

MLA Handbook (7th Edition):

Fang, Austin. “Improved Rotor Track And Balance Algorithm And System Identification Of Rotorcraft Using Flight Data .” 2015. Web. 21 Apr 2019.

Vancouver:

Fang A. Improved Rotor Track And Balance Algorithm And System Identification Of Rotorcraft Using Flight Data . [Internet] [Thesis]. Cornell University; 2015. [cited 2019 Apr 21]. Available from: http://hdl.handle.net/1813/39294.

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

Council of Science Editors:

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

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


University of Melbourne

23. Bourne, Kate. Vortex ring and rotor wake interaction with solid surfaces.

Degree: 2017, University of Melbourne

 The interaction between vortex structures and solid surfaces represents an inherently complex flow environment. When considering the rotor wake downwash generated by rotary-wing aircraft operating… (more)

Subjects/Keywords: rotor wake; vortex ring; brownout; helicopter

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APA (6th Edition):

Bourne, K. (2017). Vortex ring and rotor wake interaction with solid surfaces. (Doctoral Dissertation). University of Melbourne. Retrieved from http://hdl.handle.net/11343/192902

Chicago Manual of Style (16th Edition):

Bourne, Kate. “Vortex ring and rotor wake interaction with solid surfaces.” 2017. Doctoral Dissertation, University of Melbourne. Accessed April 21, 2019. http://hdl.handle.net/11343/192902.

MLA Handbook (7th Edition):

Bourne, Kate. “Vortex ring and rotor wake interaction with solid surfaces.” 2017. Web. 21 Apr 2019.

Vancouver:

Bourne K. Vortex ring and rotor wake interaction with solid surfaces. [Internet] [Doctoral dissertation]. University of Melbourne; 2017. [cited 2019 Apr 21]. Available from: http://hdl.handle.net/11343/192902.

Council of Science Editors:

Bourne K. Vortex ring and rotor wake interaction with solid surfaces. [Doctoral Dissertation]. University of Melbourne; 2017. Available from: http://hdl.handle.net/11343/192902


Georgia Tech

24. Battey, Luke Sterling. A hybrid Navier Stokes/vortex particle wake methodology for modeling helicopter rotors in forward flight and maneuvers.

Degree: MS, Aerospace Engineering, 2018, Georgia Tech

 Maneuvering flight and high-speed flight are critical design points in any rotorcraft’s operating envelope. These conditions give complex flow phenomena, creating high stresses and vibrations.… (more)

Subjects/Keywords: Helicopter; Rotor; Rotorcraft; Hybrid; Wake; Vortex; Particle

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APA (6th Edition):

Battey, L. S. (2018). A hybrid Navier Stokes/vortex particle wake methodology for modeling helicopter rotors in forward flight and maneuvers. (Masters Thesis). Georgia Tech. Retrieved from http://hdl.handle.net/1853/59934

Chicago Manual of Style (16th Edition):

Battey, Luke Sterling. “A hybrid Navier Stokes/vortex particle wake methodology for modeling helicopter rotors in forward flight and maneuvers.” 2018. Masters Thesis, Georgia Tech. Accessed April 21, 2019. http://hdl.handle.net/1853/59934.

MLA Handbook (7th Edition):

Battey, Luke Sterling. “A hybrid Navier Stokes/vortex particle wake methodology for modeling helicopter rotors in forward flight and maneuvers.” 2018. Web. 21 Apr 2019.

Vancouver:

Battey LS. A hybrid Navier Stokes/vortex particle wake methodology for modeling helicopter rotors in forward flight and maneuvers. [Internet] [Masters thesis]. Georgia Tech; 2018. [cited 2019 Apr 21]. Available from: http://hdl.handle.net/1853/59934.

Council of Science Editors:

Battey LS. A hybrid Navier Stokes/vortex particle wake methodology for modeling helicopter rotors in forward flight and maneuvers. [Masters Thesis]. Georgia Tech; 2018. Available from: http://hdl.handle.net/1853/59934

25. Skingle, Graham William. Structural modification using experimental data.

Degree: PhD, 1989, Imperial College London

Subjects/Keywords: 629.133; Helicopter vibrations

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APA (6th Edition):

Skingle, G. W. (1989). Structural modification using experimental data. (Doctoral Dissertation). Imperial College London. Retrieved from http://hdl.handle.net/10044/1/47664

Chicago Manual of Style (16th Edition):

Skingle, Graham William. “Structural modification using experimental data.” 1989. Doctoral Dissertation, Imperial College London. Accessed April 21, 2019. http://hdl.handle.net/10044/1/47664.

MLA Handbook (7th Edition):

Skingle, Graham William. “Structural modification using experimental data.” 1989. Web. 21 Apr 2019.

Vancouver:

Skingle GW. Structural modification using experimental data. [Internet] [Doctoral dissertation]. Imperial College London; 1989. [cited 2019 Apr 21]. Available from: http://hdl.handle.net/10044/1/47664.

Council of Science Editors:

Skingle GW. Structural modification using experimental data. [Doctoral Dissertation]. Imperial College London; 1989. Available from: http://hdl.handle.net/10044/1/47664


University of New South Wales

26. Pei, Yang. An investigation of methodologies for stochastic simulation of helicopter accidents under autorotation scenarios.

Degree: Mechanical & Manufacturing Engineering, 2016, University of New South Wales

 Traditionally investigation into helicopter accidents has focused heavily on building complex, deterministic FE models and attempting to validate them with a small number of full… (more)

Subjects/Keywords: Non-parametric analysis; Stochastic simulation; Helicopter accident

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APA (6th Edition):

Pei, Y. (2016). An investigation of methodologies for stochastic simulation of helicopter accidents under autorotation scenarios. (Doctoral Dissertation). University of New South Wales. Retrieved from http://handle.unsw.edu.au/1959.4/56911 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:42023/SOURCE02?view=true

Chicago Manual of Style (16th Edition):

Pei, Yang. “An investigation of methodologies for stochastic simulation of helicopter accidents under autorotation scenarios.” 2016. Doctoral Dissertation, University of New South Wales. Accessed April 21, 2019. http://handle.unsw.edu.au/1959.4/56911 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:42023/SOURCE02?view=true.

MLA Handbook (7th Edition):

Pei, Yang. “An investigation of methodologies for stochastic simulation of helicopter accidents under autorotation scenarios.” 2016. Web. 21 Apr 2019.

Vancouver:

Pei Y. An investigation of methodologies for stochastic simulation of helicopter accidents under autorotation scenarios. [Internet] [Doctoral dissertation]. University of New South Wales; 2016. [cited 2019 Apr 21]. Available from: http://handle.unsw.edu.au/1959.4/56911 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:42023/SOURCE02?view=true.

Council of Science Editors:

Pei Y. An investigation of methodologies for stochastic simulation of helicopter accidents under autorotation scenarios. [Doctoral Dissertation]. University of New South Wales; 2016. Available from: http://handle.unsw.edu.au/1959.4/56911 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:42023/SOURCE02?view=true


University of New South Wales

27. Khaksar, Zeinab. Numerical Modelling of the Effects of Vibration in Helicopters for Prediction and Analysis of Human Comfort Assessment.

Degree: Engineering & Information Technology Canberra, 2018, University of New South Wales

 The pilot’s situational awareness and the ability for decision making are affected by the vibration in helicopters. In addition, the vibration can also increase the… (more)

Subjects/Keywords: Helicopter vibration; Human comfort; Numerical modelling

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APA (6th Edition):

Khaksar, Z. (2018). Numerical Modelling of the Effects of Vibration in Helicopters for Prediction and Analysis of Human Comfort Assessment. (Doctoral Dissertation). University of New South Wales. Retrieved from http://handle.unsw.edu.au/1959.4/60381 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:51968/SOURCE02?view=true

Chicago Manual of Style (16th Edition):

Khaksar, Zeinab. “Numerical Modelling of the Effects of Vibration in Helicopters for Prediction and Analysis of Human Comfort Assessment.” 2018. Doctoral Dissertation, University of New South Wales. Accessed April 21, 2019. http://handle.unsw.edu.au/1959.4/60381 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:51968/SOURCE02?view=true.

MLA Handbook (7th Edition):

Khaksar, Zeinab. “Numerical Modelling of the Effects of Vibration in Helicopters for Prediction and Analysis of Human Comfort Assessment.” 2018. Web. 21 Apr 2019.

Vancouver:

Khaksar Z. Numerical Modelling of the Effects of Vibration in Helicopters for Prediction and Analysis of Human Comfort Assessment. [Internet] [Doctoral dissertation]. University of New South Wales; 2018. [cited 2019 Apr 21]. Available from: http://handle.unsw.edu.au/1959.4/60381 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:51968/SOURCE02?view=true.

Council of Science Editors:

Khaksar Z. Numerical Modelling of the Effects of Vibration in Helicopters for Prediction and Analysis of Human Comfort Assessment. [Doctoral Dissertation]. University of New South Wales; 2018. Available from: http://handle.unsw.edu.au/1959.4/60381 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:51968/SOURCE02?view=true


University of Illinois – Urbana-Champaign

28. Liu, Yitao. An integrator backstepping controller for a standard helicopter.

Degree: MS, 1200, 2010, University of Illinois – Urbana-Champaign

 This thesis investigates the use of an integrator backstepping controller for a standard helicopter. First, a dynamic model of the helicopter in hovering condition is… (more)

Subjects/Keywords: integrator backstepping controller; standard helicopter model

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APA (6th Edition):

Liu, Y. (2010). An integrator backstepping controller for a standard helicopter. (Thesis). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/16818

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):

Liu, Yitao. “An integrator backstepping controller for a standard helicopter.” 2010. Thesis, University of Illinois – Urbana-Champaign. Accessed April 21, 2019. http://hdl.handle.net/2142/16818.

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

MLA Handbook (7th Edition):

Liu, Yitao. “An integrator backstepping controller for a standard helicopter.” 2010. Web. 21 Apr 2019.

Vancouver:

Liu Y. An integrator backstepping controller for a standard helicopter. [Internet] [Thesis]. University of Illinois – Urbana-Champaign; 2010. [cited 2019 Apr 21]. Available from: http://hdl.handle.net/2142/16818.

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

Council of Science Editors:

Liu Y. An integrator backstepping controller for a standard helicopter. [Thesis]. University of Illinois – Urbana-Champaign; 2010. Available from: http://hdl.handle.net/2142/16818

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


University of Notre Dame

29. Christopher O. Porter. The Optical Environment from the Tip Vortices of a Helicopter in Different Flight Regimes</h1>.

Degree: PhD, Aerospace and Mechanical Engineering, 2011, University of Notre Dame

  Aero-optical aberrations associated with turbulent compressible flow fields can seriously degrade the performance of an optical system; the effect of these aberrations increases as… (more)

Subjects/Keywords: rotorcraft; aero-optics; helicopter; optics; directed-energy

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APA (6th Edition):

Porter, C. O. (2011). The Optical Environment from the Tip Vortices of a Helicopter in Different Flight Regimes</h1>. (Doctoral Dissertation). University of Notre Dame. Retrieved from https://curate.nd.edu/show/9s161546d84

Chicago Manual of Style (16th Edition):

Porter, Christopher O.. “The Optical Environment from the Tip Vortices of a Helicopter in Different Flight Regimes</h1>.” 2011. Doctoral Dissertation, University of Notre Dame. Accessed April 21, 2019. https://curate.nd.edu/show/9s161546d84.

MLA Handbook (7th Edition):

Porter, Christopher O.. “The Optical Environment from the Tip Vortices of a Helicopter in Different Flight Regimes</h1>.” 2011. Web. 21 Apr 2019.

Vancouver:

Porter CO. The Optical Environment from the Tip Vortices of a Helicopter in Different Flight Regimes</h1>. [Internet] [Doctoral dissertation]. University of Notre Dame; 2011. [cited 2019 Apr 21]. Available from: https://curate.nd.edu/show/9s161546d84.

Council of Science Editors:

Porter CO. The Optical Environment from the Tip Vortices of a Helicopter in Different Flight Regimes</h1>. [Doctoral Dissertation]. University of Notre Dame; 2011. Available from: https://curate.nd.edu/show/9s161546d84


Virginia Tech

30. Collins, Robert James. Design of a Helicopter Slung Vehicle for Actuated Payload Placement.

Degree: MS, Mechanical Engineering, 2012, Virginia Tech

 Helicopters have been used in applications where they need to carry a slung load for years. More recently, unmanned (UAV) helicopters are being used to… (more)

Subjects/Keywords: Tethered Payload; Helicopter; Slung Load; Autonomous Systems

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APA (6th Edition):

Collins, R. J. (2012). Design of a Helicopter Slung Vehicle for Actuated Payload Placement. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/31882

Chicago Manual of Style (16th Edition):

Collins, Robert James. “Design of a Helicopter Slung Vehicle for Actuated Payload Placement.” 2012. Masters Thesis, Virginia Tech. Accessed April 21, 2019. http://hdl.handle.net/10919/31882.

MLA Handbook (7th Edition):

Collins, Robert James. “Design of a Helicopter Slung Vehicle for Actuated Payload Placement.” 2012. Web. 21 Apr 2019.

Vancouver:

Collins RJ. Design of a Helicopter Slung Vehicle for Actuated Payload Placement. [Internet] [Masters thesis]. Virginia Tech; 2012. [cited 2019 Apr 21]. Available from: http://hdl.handle.net/10919/31882.

Council of Science Editors:

Collins RJ. Design of a Helicopter Slung Vehicle for Actuated Payload Placement. [Masters Thesis]. Virginia Tech; 2012. Available from: http://hdl.handle.net/10919/31882

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