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You searched for subject:(rotorcraft). Showing records 1 – 30 of 128 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 (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 September 19, 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. 19 Sep 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 Sep 19]. 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


Penn State University

2. Kroninger, Christopher Matthew. CHARACTERISTICS OF A ROTOR OPTIMIZED FOR HOVER AND.

Degree: MS, Aerospace Engineering, 2008, Penn State University

 A methodology has been implemented to minimize the total power consumption of a rigid hingeless rotor. The baseline rotor has a 20ft radius with both… (more)

Subjects/Keywords: circulation; optimization; rotorcraft

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APA (6th Edition):

Kroninger, C. M. (2008). CHARACTERISTICS OF A ROTOR OPTIMIZED FOR HOVER AND. (Masters Thesis). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/8408

Chicago Manual of Style (16th Edition):

Kroninger, Christopher Matthew. “CHARACTERISTICS OF A ROTOR OPTIMIZED FOR HOVER AND.” 2008. Masters Thesis, Penn State University. Accessed September 19, 2019. https://etda.libraries.psu.edu/catalog/8408.

MLA Handbook (7th Edition):

Kroninger, Christopher Matthew. “CHARACTERISTICS OF A ROTOR OPTIMIZED FOR HOVER AND.” 2008. Web. 19 Sep 2019.

Vancouver:

Kroninger CM. CHARACTERISTICS OF A ROTOR OPTIMIZED FOR HOVER AND. [Internet] [Masters thesis]. Penn State University; 2008. [cited 2019 Sep 19]. Available from: https://etda.libraries.psu.edu/catalog/8408.

Council of Science Editors:

Kroninger CM. CHARACTERISTICS OF A ROTOR OPTIMIZED FOR HOVER AND. [Masters Thesis]. Penn State University; 2008. Available from: https://etda.libraries.psu.edu/catalog/8408


Penn State University

3. Roedts II, Robert Lee. Rotorcraft Performance Enhancements Due to a Lower-Surface Miniature Effector.

Degree: MS, Aerospace Engineering, 2008, Penn State University

 Although the application of advanced structures and intelligent control systems on helicopters has seen a dramatic increase over the past two decades, the overall performance… (more)

Subjects/Keywords: performance; aerodynamics; rotorcraft

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APA (6th Edition):

Roedts II, R. L. (2008). Rotorcraft Performance Enhancements Due to a Lower-Surface Miniature Effector. (Masters Thesis). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/8829

Chicago Manual of Style (16th Edition):

Roedts II, Robert Lee. “Rotorcraft Performance Enhancements Due to a Lower-Surface Miniature Effector.” 2008. Masters Thesis, Penn State University. Accessed September 19, 2019. https://etda.libraries.psu.edu/catalog/8829.

MLA Handbook (7th Edition):

Roedts II, Robert Lee. “Rotorcraft Performance Enhancements Due to a Lower-Surface Miniature Effector.” 2008. Web. 19 Sep 2019.

Vancouver:

Roedts II RL. Rotorcraft Performance Enhancements Due to a Lower-Surface Miniature Effector. [Internet] [Masters thesis]. Penn State University; 2008. [cited 2019 Sep 19]. Available from: https://etda.libraries.psu.edu/catalog/8829.

Council of Science Editors:

Roedts II RL. Rotorcraft Performance Enhancements Due to a Lower-Surface Miniature Effector. [Masters Thesis]. Penn State University; 2008. Available from: https://etda.libraries.psu.edu/catalog/8829


Penn State University

4. Schneeberger, Grant M. ICE PROJECTILE LENGTH PREDICTION OF SHED ICE FROM ROTOR BLADES.

Degree: MS, Aerospace Engineering, 2016, Penn State University

 Ice shed from rotor blades can be a ballistic concern for conventional helicopters, tiltrotors, wind turbines, and propellers. In conventional helicopters these ice projectiles can… (more)

Subjects/Keywords: ice; rotorcraft; shedding

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APA (6th Edition):

Schneeberger, G. M. (2016). ICE PROJECTILE LENGTH PREDICTION OF SHED ICE FROM ROTOR BLADES. (Masters Thesis). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/13562gms5247

Chicago Manual of Style (16th Edition):

Schneeberger, Grant M. “ICE PROJECTILE LENGTH PREDICTION OF SHED ICE FROM ROTOR BLADES.” 2016. Masters Thesis, Penn State University. Accessed September 19, 2019. https://etda.libraries.psu.edu/catalog/13562gms5247.

MLA Handbook (7th Edition):

Schneeberger, Grant M. “ICE PROJECTILE LENGTH PREDICTION OF SHED ICE FROM ROTOR BLADES.” 2016. Web. 19 Sep 2019.

Vancouver:

Schneeberger GM. ICE PROJECTILE LENGTH PREDICTION OF SHED ICE FROM ROTOR BLADES. [Internet] [Masters thesis]. Penn State University; 2016. [cited 2019 Sep 19]. Available from: https://etda.libraries.psu.edu/catalog/13562gms5247.

Council of Science Editors:

Schneeberger GM. ICE PROJECTILE LENGTH PREDICTION OF SHED ICE FROM ROTOR BLADES. [Masters Thesis]. Penn State University; 2016. Available from: https://etda.libraries.psu.edu/catalog/13562gms5247


Penn State University

5. Santarelli, David. An Energy Harvesting Device for Powering Rotor Load Monitoring Sensors.

Degree: MS, Mechanical Engineering, 2010, Penn State University

 Health and Usage Monitoring Systems (HUMS) on helicopters help to determine when dynamic, flight critical components are replaced. These systems work on the principle of… (more)

Subjects/Keywords: Energy Harvesting; Rotorcraft; Loads Monitoring

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APA (6th Edition):

Santarelli, D. (2010). An Energy Harvesting Device for Powering Rotor Load Monitoring Sensors. (Masters Thesis). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/9984

Chicago Manual of Style (16th Edition):

Santarelli, David. “An Energy Harvesting Device for Powering Rotor Load Monitoring Sensors.” 2010. Masters Thesis, Penn State University. Accessed September 19, 2019. https://etda.libraries.psu.edu/catalog/9984.

MLA Handbook (7th Edition):

Santarelli, David. “An Energy Harvesting Device for Powering Rotor Load Monitoring Sensors.” 2010. Web. 19 Sep 2019.

Vancouver:

Santarelli D. An Energy Harvesting Device for Powering Rotor Load Monitoring Sensors. [Internet] [Masters thesis]. Penn State University; 2010. [cited 2019 Sep 19]. Available from: https://etda.libraries.psu.edu/catalog/9984.

Council of Science Editors:

Santarelli D. An Energy Harvesting Device for Powering Rotor Load Monitoring Sensors. [Masters Thesis]. Penn State University; 2010. Available from: https://etda.libraries.psu.edu/catalog/9984


Penn State University

6. Hennes, Christopher Conrad. Computation of Interactional Aerodynamics for Noise Prediction of Heavy Lift Rotorcraft.

Degree: PhD, Aerospace Engineering, 2013, Penn State University

 Many computational tools are used when developing a modern helicopter. As the design space is narrowed, more accurate and time-intensive tools are brought to bear.… (more)

Subjects/Keywords: Acoustics; Rotorcraft; Computational Fluid Dynamics

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APA (6th Edition):

Hennes, C. C. (2013). Computation of Interactional Aerodynamics for Noise Prediction of Heavy Lift Rotorcraft. (Doctoral Dissertation). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/19604

Chicago Manual of Style (16th Edition):

Hennes, Christopher Conrad. “Computation of Interactional Aerodynamics for Noise Prediction of Heavy Lift Rotorcraft.” 2013. Doctoral Dissertation, Penn State University. Accessed September 19, 2019. https://etda.libraries.psu.edu/catalog/19604.

MLA Handbook (7th Edition):

Hennes, Christopher Conrad. “Computation of Interactional Aerodynamics for Noise Prediction of Heavy Lift Rotorcraft.” 2013. Web. 19 Sep 2019.

Vancouver:

Hennes CC. Computation of Interactional Aerodynamics for Noise Prediction of Heavy Lift Rotorcraft. [Internet] [Doctoral dissertation]. Penn State University; 2013. [cited 2019 Sep 19]. Available from: https://etda.libraries.psu.edu/catalog/19604.

Council of Science Editors:

Hennes CC. Computation of Interactional Aerodynamics for Noise Prediction of Heavy Lift Rotorcraft. [Doctoral Dissertation]. Penn State University; 2013. Available from: https://etda.libraries.psu.edu/catalog/19604


Penn State University

7. Mahmood, Raheel Sheikh. Vibration energy harvesting from rotorcraft drive systems using thermoelectric conversion of heat generated by mechanical damping.

Degree: MS, Aerospace Engineering, 2014, Penn State University

 Energy harvesting from ambient structural vibrations on rotorcraft continues to generate increasing interest due to its potential use in powering wireless sensors for applications such… (more)

Subjects/Keywords: energy harvesting; vibration; rotorcraft

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APA (6th Edition):

Mahmood, R. S. (2014). Vibration energy harvesting from rotorcraft drive systems using thermoelectric conversion of heat generated by mechanical damping. (Masters Thesis). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/23693

Chicago Manual of Style (16th Edition):

Mahmood, Raheel Sheikh. “Vibration energy harvesting from rotorcraft drive systems using thermoelectric conversion of heat generated by mechanical damping.” 2014. Masters Thesis, Penn State University. Accessed September 19, 2019. https://etda.libraries.psu.edu/catalog/23693.

MLA Handbook (7th Edition):

Mahmood, Raheel Sheikh. “Vibration energy harvesting from rotorcraft drive systems using thermoelectric conversion of heat generated by mechanical damping.” 2014. Web. 19 Sep 2019.

Vancouver:

Mahmood RS. Vibration energy harvesting from rotorcraft drive systems using thermoelectric conversion of heat generated by mechanical damping. [Internet] [Masters thesis]. Penn State University; 2014. [cited 2019 Sep 19]. Available from: https://etda.libraries.psu.edu/catalog/23693.

Council of Science Editors:

Mahmood RS. Vibration energy harvesting from rotorcraft drive systems using thermoelectric conversion of heat generated by mechanical damping. [Masters Thesis]. Penn State University; 2014. Available from: https://etda.libraries.psu.edu/catalog/23693


Cranfield University

8. Place, C. S. Modelling of multiple failure mechanisms for system reliability prediction.

Degree: PhD, 2002, Cranfield University

 Helicopters are highly dependent on their transmission systems, which provide the vital links from the engines to the rotor and ancillary systems. Components are highly… (more)

Subjects/Keywords: 629; Rotorcraft

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APA (6th Edition):

Place, C. S. (2002). Modelling of multiple failure mechanisms for system reliability prediction. (Doctoral Dissertation). Cranfield University. Retrieved from http://dspace.lib.cranfield.ac.uk/handle/1826/3320 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.248509

Chicago Manual of Style (16th Edition):

Place, C S. “Modelling of multiple failure mechanisms for system reliability prediction.” 2002. Doctoral Dissertation, Cranfield University. Accessed September 19, 2019. http://dspace.lib.cranfield.ac.uk/handle/1826/3320 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.248509.

MLA Handbook (7th Edition):

Place, C S. “Modelling of multiple failure mechanisms for system reliability prediction.” 2002. Web. 19 Sep 2019.

Vancouver:

Place CS. Modelling of multiple failure mechanisms for system reliability prediction. [Internet] [Doctoral dissertation]. Cranfield University; 2002. [cited 2019 Sep 19]. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/3320 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.248509.

Council of Science Editors:

Place CS. Modelling of multiple failure mechanisms for system reliability prediction. [Doctoral Dissertation]. Cranfield University; 2002. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/3320 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.248509


Virginia Tech

9. Hardwick, Jonathan Robert. Synthesis of Noise from Flyover Data.

Degree: MS, Mechanical Engineering, 2014, Virginia Tech

 Flyover noise is a problem that affects citizens, primarily those that live near or around places with high air traffic such as airports or military… (more)

Subjects/Keywords: rotorcraft; synthesis; flyover noise

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APA (6th Edition):

Hardwick, J. R. (2014). Synthesis of Noise from Flyover Data. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/50531

Chicago Manual of Style (16th Edition):

Hardwick, Jonathan Robert. “Synthesis of Noise from Flyover Data.” 2014. Masters Thesis, Virginia Tech. Accessed September 19, 2019. http://hdl.handle.net/10919/50531.

MLA Handbook (7th Edition):

Hardwick, Jonathan Robert. “Synthesis of Noise from Flyover Data.” 2014. Web. 19 Sep 2019.

Vancouver:

Hardwick JR. Synthesis of Noise from Flyover Data. [Internet] [Masters thesis]. Virginia Tech; 2014. [cited 2019 Sep 19]. Available from: http://hdl.handle.net/10919/50531.

Council of Science Editors:

Hardwick JR. Synthesis of Noise from Flyover Data. [Masters Thesis]. Virginia Tech; 2014. Available from: http://hdl.handle.net/10919/50531


Penn State University

10. Reich, David. Experimental Investigation of A Helicopter Rotor Hub Flow.

Degree: 2017, Penn State University

 The rotor hub system is by far the largest contributor to helicopter parasite drag and a barrier to increasing helicopter forward-flight speed and range. Additionally,… (more)

Subjects/Keywords: Helicopter; Rotorcraft; Aerodynamics; Rotor Hub; Hub Drag; Rotor Hub Drag; Rotorcraft Aerodynamics; Rotorcraft Aeromechanics; Unsteady Aerodynamics

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APA (6th Edition):

Reich, D. (2017). Experimental Investigation of A Helicopter Rotor Hub Flow. (Thesis). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/14509dbr141

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):

Reich, David. “Experimental Investigation of A Helicopter Rotor Hub Flow.” 2017. Thesis, Penn State University. Accessed September 19, 2019. https://etda.libraries.psu.edu/catalog/14509dbr141.

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

MLA Handbook (7th Edition):

Reich, David. “Experimental Investigation of A Helicopter Rotor Hub Flow.” 2017. Web. 19 Sep 2019.

Vancouver:

Reich D. Experimental Investigation of A Helicopter Rotor Hub Flow. [Internet] [Thesis]. Penn State University; 2017. [cited 2019 Sep 19]. Available from: https://etda.libraries.psu.edu/catalog/14509dbr141.

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

Council of Science Editors:

Reich D. Experimental Investigation of A Helicopter Rotor Hub Flow. [Thesis]. Penn State University; 2017. Available from: https://etda.libraries.psu.edu/catalog/14509dbr141

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


Penn State University

11. Marlow, Sean Quinn. Local Terrain Mapping for Obstacle Avoidance using Monocular Vision.

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

 The motivation behind the research described in this thesis is to be able to navigate a small unmanned aerial vehicle (UAV) through complex environments. Missions… (more)

Subjects/Keywords: occupancy grid; optical flow; obstacle avoidance; rotorcraft

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APA (6th Edition):

Marlow, S. Q. (2009). Local Terrain Mapping for Obstacle Avoidance using Monocular Vision. (Masters Thesis). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/9669

Chicago Manual of Style (16th Edition):

Marlow, Sean Quinn. “Local Terrain Mapping for Obstacle Avoidance using Monocular Vision.” 2009. Masters Thesis, Penn State University. Accessed September 19, 2019. https://etda.libraries.psu.edu/catalog/9669.

MLA Handbook (7th Edition):

Marlow, Sean Quinn. “Local Terrain Mapping for Obstacle Avoidance using Monocular Vision.” 2009. Web. 19 Sep 2019.

Vancouver:

Marlow SQ. Local Terrain Mapping for Obstacle Avoidance using Monocular Vision. [Internet] [Masters thesis]. Penn State University; 2009. [cited 2019 Sep 19]. Available from: https://etda.libraries.psu.edu/catalog/9669.

Council of Science Editors:

Marlow SQ. Local Terrain Mapping for Obstacle Avoidance using Monocular Vision. [Masters Thesis]. Penn State University; 2009. Available from: https://etda.libraries.psu.edu/catalog/9669


Penn State University

12. Cormier, Christopher. DESIGN OF A CENTRIFUGE AND AERODYNAMIC TESTING APPARATUS FOR EVALUATING THE PERFORMANCE OF A NOVEL TRAILING-EDGE FLAP ACTUATOR.

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

 Primary helicopter flight control generally involves exposed, high-maintenance equipment such as bearings, linkages, hinges, and swashplates. Though these mechanisms are necessary for helicopter flight performance,… (more)

Subjects/Keywords: individual blade control; centrifuge; smart materials; rotorcraft

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APA (6th Edition):

Cormier, C. (2009). DESIGN OF A CENTRIFUGE AND AERODYNAMIC TESTING APPARATUS FOR EVALUATING THE PERFORMANCE OF A NOVEL TRAILING-EDGE FLAP ACTUATOR. (Masters Thesis). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/9071

Chicago Manual of Style (16th Edition):

Cormier, Christopher. “DESIGN OF A CENTRIFUGE AND AERODYNAMIC TESTING APPARATUS FOR EVALUATING THE PERFORMANCE OF A NOVEL TRAILING-EDGE FLAP ACTUATOR.” 2009. Masters Thesis, Penn State University. Accessed September 19, 2019. https://etda.libraries.psu.edu/catalog/9071.

MLA Handbook (7th Edition):

Cormier, Christopher. “DESIGN OF A CENTRIFUGE AND AERODYNAMIC TESTING APPARATUS FOR EVALUATING THE PERFORMANCE OF A NOVEL TRAILING-EDGE FLAP ACTUATOR.” 2009. Web. 19 Sep 2019.

Vancouver:

Cormier C. DESIGN OF A CENTRIFUGE AND AERODYNAMIC TESTING APPARATUS FOR EVALUATING THE PERFORMANCE OF A NOVEL TRAILING-EDGE FLAP ACTUATOR. [Internet] [Masters thesis]. Penn State University; 2009. [cited 2019 Sep 19]. Available from: https://etda.libraries.psu.edu/catalog/9071.

Council of Science Editors:

Cormier C. DESIGN OF A CENTRIFUGE AND AERODYNAMIC TESTING APPARATUS FOR EVALUATING THE PERFORMANCE OF A NOVEL TRAILING-EDGE FLAP ACTUATOR. [Masters Thesis]. Penn State University; 2009. Available from: https://etda.libraries.psu.edu/catalog/9071


Penn State University

13. 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 September 19, 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. 19 Sep 2019.

Vancouver:

Caudle DB. Damage Mitigation for Rotorcraft through Load Alleviating Control. [Internet] [Masters thesis]. Penn State University; 2014. [cited 2019 Sep 19]. 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


Virginia Tech

14. Cooper, Jared K. Modeling of a Small-Scale Remote Controllable Helicopter for Simulation and Control Development.

Degree: MS, Mechanical Engineering, 2006, Virginia Tech

 Abstract The Virginia Polytechnic Institute and State University has recently expanded its unmanned and autonomous systems research to include aerial vehicles. In the summer of… (more)

Subjects/Keywords: rotorcraft; modeling; simulation

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APA (6th Edition):

Cooper, J. K. (2006). Modeling of a Small-Scale Remote Controllable Helicopter for Simulation and Control Development. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/41891

Chicago Manual of Style (16th Edition):

Cooper, Jared K. “Modeling of a Small-Scale Remote Controllable Helicopter for Simulation and Control Development.” 2006. Masters Thesis, Virginia Tech. Accessed September 19, 2019. http://hdl.handle.net/10919/41891.

MLA Handbook (7th Edition):

Cooper, Jared K. “Modeling of a Small-Scale Remote Controllable Helicopter for Simulation and Control Development.” 2006. Web. 19 Sep 2019.

Vancouver:

Cooper JK. Modeling of a Small-Scale Remote Controllable Helicopter for Simulation and Control Development. [Internet] [Masters thesis]. Virginia Tech; 2006. [cited 2019 Sep 19]. Available from: http://hdl.handle.net/10919/41891.

Council of Science Editors:

Cooper JK. Modeling of a Small-Scale Remote Controllable Helicopter for Simulation and Control Development. [Masters Thesis]. Virginia Tech; 2006. Available from: http://hdl.handle.net/10919/41891


Cranfield University

15. Ruge Montilla, Jhonn Hamberth. Modelling of tilt rotor mission performance to assess environmental impact.

Degree: MSc by Research, 2012, Cranfield University

 New technologies and new rotorcraft operations are being developed in order to meet new environmental requirements such as noise reduction and less pollutant emissions. In… (more)

Subjects/Keywords: Rotorcraft; Mission Level; Atmosphere; Pollutant Emissions; Model

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APA (6th Edition):

Ruge Montilla, J. H. (2012). Modelling of tilt rotor mission performance to assess environmental impact. (Masters Thesis). Cranfield University. Retrieved from http://dspace.lib.cranfield.ac.uk/handle/1826/7292

Chicago Manual of Style (16th Edition):

Ruge Montilla, Jhonn Hamberth. “Modelling of tilt rotor mission performance to assess environmental impact.” 2012. Masters Thesis, Cranfield University. Accessed September 19, 2019. http://dspace.lib.cranfield.ac.uk/handle/1826/7292.

MLA Handbook (7th Edition):

Ruge Montilla, Jhonn Hamberth. “Modelling of tilt rotor mission performance to assess environmental impact.” 2012. Web. 19 Sep 2019.

Vancouver:

Ruge Montilla JH. Modelling of tilt rotor mission performance to assess environmental impact. [Internet] [Masters thesis]. Cranfield University; 2012. [cited 2019 Sep 19]. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/7292.

Council of Science Editors:

Ruge Montilla JH. Modelling of tilt rotor mission performance to assess environmental impact. [Masters Thesis]. Cranfield University; 2012. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/7292


Delft University of Technology

16. Van Gool, P.C.A. Rotorcraft responses to atmospheric turbulence.

Degree: 1997, Delft University of Technology

Subjects/Keywords: rotorcraft; turbulence; simulation

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APA (6th Edition):

Van Gool, P. C. A. (1997). Rotorcraft responses to atmospheric turbulence. (Doctoral Dissertation). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:2fa59b2d-8131-4608-9eb8-61b256603516 ; urn:NBN:nl:ui:24-uuid:2fa59b2d-8131-4608-9eb8-61b256603516 ; urn:NBN:nl:ui:24-uuid:2fa59b2d-8131-4608-9eb8-61b256603516 ; http://resolver.tudelft.nl/uuid:2fa59b2d-8131-4608-9eb8-61b256603516

Chicago Manual of Style (16th Edition):

Van Gool, P C A. “Rotorcraft responses to atmospheric turbulence.” 1997. Doctoral Dissertation, Delft University of Technology. Accessed September 19, 2019. http://resolver.tudelft.nl/uuid:2fa59b2d-8131-4608-9eb8-61b256603516 ; urn:NBN:nl:ui:24-uuid:2fa59b2d-8131-4608-9eb8-61b256603516 ; urn:NBN:nl:ui:24-uuid:2fa59b2d-8131-4608-9eb8-61b256603516 ; http://resolver.tudelft.nl/uuid:2fa59b2d-8131-4608-9eb8-61b256603516.

MLA Handbook (7th Edition):

Van Gool, P C A. “Rotorcraft responses to atmospheric turbulence.” 1997. Web. 19 Sep 2019.

Vancouver:

Van Gool PCA. Rotorcraft responses to atmospheric turbulence. [Internet] [Doctoral dissertation]. Delft University of Technology; 1997. [cited 2019 Sep 19]. Available from: http://resolver.tudelft.nl/uuid:2fa59b2d-8131-4608-9eb8-61b256603516 ; urn:NBN:nl:ui:24-uuid:2fa59b2d-8131-4608-9eb8-61b256603516 ; urn:NBN:nl:ui:24-uuid:2fa59b2d-8131-4608-9eb8-61b256603516 ; http://resolver.tudelft.nl/uuid:2fa59b2d-8131-4608-9eb8-61b256603516.

Council of Science Editors:

Van Gool PCA. Rotorcraft responses to atmospheric turbulence. [Doctoral Dissertation]. Delft University of Technology; 1997. Available from: http://resolver.tudelft.nl/uuid:2fa59b2d-8131-4608-9eb8-61b256603516 ; urn:NBN:nl:ui:24-uuid:2fa59b2d-8131-4608-9eb8-61b256603516 ; urn:NBN:nl:ui:24-uuid:2fa59b2d-8131-4608-9eb8-61b256603516 ; http://resolver.tudelft.nl/uuid:2fa59b2d-8131-4608-9eb8-61b256603516


Cornell University

17. 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 September 19, 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. 19 Sep 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 Sep 19]. 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


Georgia Tech

18. 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 September 19, 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. 19 Sep 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 Sep 19]. 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


Iowa State University

19. Ghosh, Sayan. Configurational effect on dust cloud formation and brownout.

Degree: 2010, Iowa State University

Rotorcraft brownout is in-flight visibility restriction caused by clouds of sand and dust particles during landing, take off, and near ground flight operations in arid… (more)

Subjects/Keywords: Brownout; CFD; Configuration; Dust; Rotorcraft; Aerospace Engineering

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APA (6th Edition):

Ghosh, S. (2010). Configurational effect on dust cloud formation and brownout. (Thesis). Iowa State University. Retrieved from https://lib.dr.iastate.edu/etd/11489

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):

Ghosh, Sayan. “Configurational effect on dust cloud formation and brownout.” 2010. Thesis, Iowa State University. Accessed September 19, 2019. https://lib.dr.iastate.edu/etd/11489.

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

MLA Handbook (7th Edition):

Ghosh, Sayan. “Configurational effect on dust cloud formation and brownout.” 2010. Web. 19 Sep 2019.

Vancouver:

Ghosh S. Configurational effect on dust cloud formation and brownout. [Internet] [Thesis]. Iowa State University; 2010. [cited 2019 Sep 19]. Available from: https://lib.dr.iastate.edu/etd/11489.

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

Council of Science Editors:

Ghosh S. Configurational effect on dust cloud formation and brownout. [Thesis]. Iowa State University; 2010. Available from: https://lib.dr.iastate.edu/etd/11489

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


University of Illinois – Urbana-Champaign

20. Hong, Je Won. Analysis of fountain effect for tiltrotor configuration using computational fluid simulation and experimental method.

Degree: MS, Aerospace Engineering, 2017, University of Illinois – Urbana-Champaign

 The study involves a tiltrotor’s wing/rotor configuration design to properly test the model in both hover flight condition and crosswind condition replicated in the wind… (more)

Subjects/Keywords: Tiltrotor; Fountain effect; Subsonic; Rotorcraft; Aerodynamics

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APA (6th Edition):

Hong, J. W. (2017). Analysis of fountain effect for tiltrotor configuration using computational fluid simulation and experimental method. (Thesis). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/97452

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):

Hong, Je Won. “Analysis of fountain effect for tiltrotor configuration using computational fluid simulation and experimental method.” 2017. Thesis, University of Illinois – Urbana-Champaign. Accessed September 19, 2019. http://hdl.handle.net/2142/97452.

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

MLA Handbook (7th Edition):

Hong, Je Won. “Analysis of fountain effect for tiltrotor configuration using computational fluid simulation and experimental method.” 2017. Web. 19 Sep 2019.

Vancouver:

Hong JW. Analysis of fountain effect for tiltrotor configuration using computational fluid simulation and experimental method. [Internet] [Thesis]. University of Illinois – Urbana-Champaign; 2017. [cited 2019 Sep 19]. Available from: http://hdl.handle.net/2142/97452.

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

Council of Science Editors:

Hong JW. Analysis of fountain effect for tiltrotor configuration using computational fluid simulation and experimental method. [Thesis]. University of Illinois – Urbana-Champaign; 2017. Available from: http://hdl.handle.net/2142/97452

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


University of Notre Dame

21. 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 September 19, 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. 19 Sep 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 Sep 19]. 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


Georgia Tech

22. Scott, Robert C. A new rotorcraft design framework based on reliability and cost.

Degree: PhD, Aerospace Engineering, 2016, Georgia Tech

 Helicopters provide essential services in civil and military applications due to their multirole capability and operational flexibility, but the combination of the disparate performance conditions… (more)

Subjects/Keywords: Rotorcraft design; Aircraft design; Rotorcraft assessment; Conceptual design and assessment; Life-cycle cost; Reliability; Maintainability

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APA (6th Edition):

Scott, R. C. (2016). A new rotorcraft design framework based on reliability and cost. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/55640

Chicago Manual of Style (16th Edition):

Scott, Robert C. “A new rotorcraft design framework based on reliability and cost.” 2016. Doctoral Dissertation, Georgia Tech. Accessed September 19, 2019. http://hdl.handle.net/1853/55640.

MLA Handbook (7th Edition):

Scott, Robert C. “A new rotorcraft design framework based on reliability and cost.” 2016. Web. 19 Sep 2019.

Vancouver:

Scott RC. A new rotorcraft design framework based on reliability and cost. [Internet] [Doctoral dissertation]. Georgia Tech; 2016. [cited 2019 Sep 19]. Available from: http://hdl.handle.net/1853/55640.

Council of Science Editors:

Scott RC. A new rotorcraft design framework based on reliability and cost. [Doctoral Dissertation]. Georgia Tech; 2016. Available from: http://hdl.handle.net/1853/55640


Penn State University

23. Scarborough, Lloyd Harmon. Dynamics of Fluidic Devices with Applications to Rotor Pitch Links.

Degree: PhD, Mechanical Engineering, 2014, Penn State University

 Coupling a Fluidic Flexible Matrix Composite (F2MC) to an air-pressurized fluid port produces a fundamentally new class of tunable vibration isolator. This fluidlastic device provides… (more)

Subjects/Keywords: vibration isolation; pitch link loads; fluidic pitch link; rotorcraft vibration; helicopter vibration; rotorcraft performance

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APA (6th Edition):

Scarborough, L. H. (2014). Dynamics of Fluidic Devices with Applications to Rotor Pitch Links. (Doctoral Dissertation). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/20438

Chicago Manual of Style (16th Edition):

Scarborough, Lloyd Harmon. “Dynamics of Fluidic Devices with Applications to Rotor Pitch Links.” 2014. Doctoral Dissertation, Penn State University. Accessed September 19, 2019. https://etda.libraries.psu.edu/catalog/20438.

MLA Handbook (7th Edition):

Scarborough, Lloyd Harmon. “Dynamics of Fluidic Devices with Applications to Rotor Pitch Links.” 2014. Web. 19 Sep 2019.

Vancouver:

Scarborough LH. Dynamics of Fluidic Devices with Applications to Rotor Pitch Links. [Internet] [Doctoral dissertation]. Penn State University; 2014. [cited 2019 Sep 19]. Available from: https://etda.libraries.psu.edu/catalog/20438.

Council of Science Editors:

Scarborough LH. Dynamics of Fluidic Devices with Applications to Rotor Pitch Links. [Doctoral Dissertation]. Penn State University; 2014. Available from: https://etda.libraries.psu.edu/catalog/20438


Indian Institute of Science

24. Kumar, Rajan. A Neural Network Approach To Rotorcraft Parameter Estimation.

Degree: 2007, Indian Institute of Science

 The present work focuses on the system identification method of aerodynamic parameter estimation which is used to calculate the stability and control derivatives required for… (more)

Subjects/Keywords: Airplanes - Rotors; Neural Networks; Aerodynamic Parameter Estimation; Rotorcraft Flight Mechanics; Rotorcraft - Simulation; Rotorcraft - System Identification; Artificial Neural Network (ANN); Radial Basis Function Network (RBFN); Multilayer Perceptron (MLP); Real Time Flight Data; Rotorcraft Parameter Estimation; Aeronautics

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APA (6th Edition):

Kumar, R. (2007). A Neural Network Approach To Rotorcraft Parameter Estimation. (Thesis). Indian Institute of Science. Retrieved from http://hdl.handle.net/2005/549

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):

Kumar, Rajan. “A Neural Network Approach To Rotorcraft Parameter Estimation.” 2007. Thesis, Indian Institute of Science. Accessed September 19, 2019. http://hdl.handle.net/2005/549.

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

MLA Handbook (7th Edition):

Kumar, Rajan. “A Neural Network Approach To Rotorcraft Parameter Estimation.” 2007. Web. 19 Sep 2019.

Vancouver:

Kumar R. A Neural Network Approach To Rotorcraft Parameter Estimation. [Internet] [Thesis]. Indian Institute of Science; 2007. [cited 2019 Sep 19]. Available from: http://hdl.handle.net/2005/549.

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

Council of Science Editors:

Kumar R. A Neural Network Approach To Rotorcraft Parameter Estimation. [Thesis]. Indian Institute of Science; 2007. Available from: http://hdl.handle.net/2005/549

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


The Ohio State University

25. Kumar, Pradeep. Development of a Single-shot Lifetime PSP Measurement Technique for Rotating Surfaces.

Degree: MS, Aero/Astro Engineering, 2010, The Ohio State University

  In this work, the viability of using pressure-sensitive paints as a pressure sensor on rotating surfaces with unsteady pressure fluctuations has been investigated. A… (more)

Subjects/Keywords: Mechanical Engineering; PSP; single-shot; lifetime; measurements; rotating surfaces; rotorcraft

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APA (6th Edition):

Kumar, P. (2010). Development of a Single-shot Lifetime PSP Measurement Technique for Rotating Surfaces. (Masters Thesis). The Ohio State University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=osu1285044595

Chicago Manual of Style (16th Edition):

Kumar, Pradeep. “Development of a Single-shot Lifetime PSP Measurement Technique for Rotating Surfaces.” 2010. Masters Thesis, The Ohio State University. Accessed September 19, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=osu1285044595.

MLA Handbook (7th Edition):

Kumar, Pradeep. “Development of a Single-shot Lifetime PSP Measurement Technique for Rotating Surfaces.” 2010. Web. 19 Sep 2019.

Vancouver:

Kumar P. Development of a Single-shot Lifetime PSP Measurement Technique for Rotating Surfaces. [Internet] [Masters thesis]. The Ohio State University; 2010. [cited 2019 Sep 19]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1285044595.

Council of Science Editors:

Kumar P. Development of a Single-shot Lifetime PSP Measurement Technique for Rotating Surfaces. [Masters Thesis]. The Ohio State University; 2010. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1285044595


Georgia Tech

26. Prosser, Daniel T. Advanced computational techniques for unsteady aerodynamic-dynamic interactions of bluff bodies.

Degree: PhD, Aerospace Engineering, 2015, Georgia Tech

 Interactions between the aerodynamics and dynamics of bluff bodies are important in many engineering applications, including suspension bridges, tall buildings, oil platforms, wind turbine towers,… (more)

Subjects/Keywords: Computational fluid dynamics; Reduced-order modeling; Tethered loads; Rotorcraft; Bluff bodies

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APA (6th Edition):

Prosser, D. T. (2015). Advanced computational techniques for unsteady aerodynamic-dynamic interactions of bluff bodies. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/53899

Chicago Manual of Style (16th Edition):

Prosser, Daniel T. “Advanced computational techniques for unsteady aerodynamic-dynamic interactions of bluff bodies.” 2015. Doctoral Dissertation, Georgia Tech. Accessed September 19, 2019. http://hdl.handle.net/1853/53899.

MLA Handbook (7th Edition):

Prosser, Daniel T. “Advanced computational techniques for unsteady aerodynamic-dynamic interactions of bluff bodies.” 2015. Web. 19 Sep 2019.

Vancouver:

Prosser DT. Advanced computational techniques for unsteady aerodynamic-dynamic interactions of bluff bodies. [Internet] [Doctoral dissertation]. Georgia Tech; 2015. [cited 2019 Sep 19]. Available from: http://hdl.handle.net/1853/53899.

Council of Science Editors:

Prosser DT. Advanced computational techniques for unsteady aerodynamic-dynamic interactions of bluff bodies. [Doctoral Dissertation]. Georgia Tech; 2015. Available from: http://hdl.handle.net/1853/53899


Penn State University

27. Bailey, Matthew John. Modeling and experimental testing of a centrifugally powered pneumatic de-icing system for rotor blades.

Degree: MS, Aerospace Engineering, 2015, Penn State University

 The goal of this research was to test, evaluate, and model a novel pneumatic approach to protect helicopter rotor blades from ice accretion. The system… (more)

Subjects/Keywords: Deicing; Deicer; Icing; Pneumatic; Rotorcraft; AERTS; Helicopter; Centrifugal

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APA (6th Edition):

Bailey, M. J. (2015). Modeling and experimental testing of a centrifugally powered pneumatic de-icing system for rotor blades. (Masters Thesis). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/23320

Chicago Manual of Style (16th Edition):

Bailey, Matthew John. “Modeling and experimental testing of a centrifugally powered pneumatic de-icing system for rotor blades.” 2015. Masters Thesis, Penn State University. Accessed September 19, 2019. https://etda.libraries.psu.edu/catalog/23320.

MLA Handbook (7th Edition):

Bailey, Matthew John. “Modeling and experimental testing of a centrifugally powered pneumatic de-icing system for rotor blades.” 2015. Web. 19 Sep 2019.

Vancouver:

Bailey MJ. Modeling and experimental testing of a centrifugally powered pneumatic de-icing system for rotor blades. [Internet] [Masters thesis]. Penn State University; 2015. [cited 2019 Sep 19]. Available from: https://etda.libraries.psu.edu/catalog/23320.

Council of Science Editors:

Bailey MJ. Modeling and experimental testing of a centrifugally powered pneumatic de-icing system for rotor blades. [Masters Thesis]. Penn State University; 2015. Available from: https://etda.libraries.psu.edu/catalog/23320


Penn State University

28. Li, Zuqun. coordinated transport of a slung load by a team of autonomous rotorcraft.

Degree: MS, Aerospace Engineering, 2014, Penn State University

 This research is motivated by the significant economical efficiency of multilift system for carrying a single heavy payload, which includes both military and commercial cargo.… (more)

Subjects/Keywords: multilift; OBTLC; coordinated transport; autonomous rotorcraft; slung load

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APA (6th Edition):

Li, Z. (2014). coordinated transport of a slung load by a team of autonomous rotorcraft. (Masters Thesis). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/23507

Chicago Manual of Style (16th Edition):

Li, Zuqun. “coordinated transport of a slung load by a team of autonomous rotorcraft.” 2014. Masters Thesis, Penn State University. Accessed September 19, 2019. https://etda.libraries.psu.edu/catalog/23507.

MLA Handbook (7th Edition):

Li, Zuqun. “coordinated transport of a slung load by a team of autonomous rotorcraft.” 2014. Web. 19 Sep 2019.

Vancouver:

Li Z. coordinated transport of a slung load by a team of autonomous rotorcraft. [Internet] [Masters thesis]. Penn State University; 2014. [cited 2019 Sep 19]. Available from: https://etda.libraries.psu.edu/catalog/23507.

Council of Science Editors:

Li Z. coordinated transport of a slung load by a team of autonomous rotorcraft. [Masters Thesis]. Penn State University; 2014. Available from: https://etda.libraries.psu.edu/catalog/23507


Penn State University

29. Shin, Bong Gun. PREDICTION OF SAND PARTICLE TRAJECTORIES AND SAND EROSION DAMAGE ON HELICOPTER ROTOR BLADES.

Degree: PhD, Aerospace Engineering, 2010, Penn State University

 Erosion damage on a helicopter rotor blade by the impact of solid particle causes serious material removal from the surface of the rotor blade. The… (more)

Subjects/Keywords: Rotorcraft; Aerodynamics; Particle Trajectory; Sand Erosion; Helicopter rotor blade

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APA (6th Edition):

Shin, B. G. (2010). PREDICTION OF SAND PARTICLE TRAJECTORIES AND SAND EROSION DAMAGE ON HELICOPTER ROTOR BLADES. (Doctoral Dissertation). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/10860

Chicago Manual of Style (16th Edition):

Shin, Bong Gun. “PREDICTION OF SAND PARTICLE TRAJECTORIES AND SAND EROSION DAMAGE ON HELICOPTER ROTOR BLADES.” 2010. Doctoral Dissertation, Penn State University. Accessed September 19, 2019. https://etda.libraries.psu.edu/catalog/10860.

MLA Handbook (7th Edition):

Shin, Bong Gun. “PREDICTION OF SAND PARTICLE TRAJECTORIES AND SAND EROSION DAMAGE ON HELICOPTER ROTOR BLADES.” 2010. Web. 19 Sep 2019.

Vancouver:

Shin BG. PREDICTION OF SAND PARTICLE TRAJECTORIES AND SAND EROSION DAMAGE ON HELICOPTER ROTOR BLADES. [Internet] [Doctoral dissertation]. Penn State University; 2010. [cited 2019 Sep 19]. Available from: https://etda.libraries.psu.edu/catalog/10860.

Council of Science Editors:

Shin BG. PREDICTION OF SAND PARTICLE TRAJECTORIES AND SAND EROSION DAMAGE ON HELICOPTER ROTOR BLADES. [Doctoral Dissertation]. Penn State University; 2010. Available from: https://etda.libraries.psu.edu/catalog/10860


Penn State University

30. Ozdemir, Gurbuz Taha. In-flight Performance Optimization for Rotorcraft with Redundant Controls.

Degree: PhD, Aerospace Engineering, 2013, Penn State University

 A conventional helicopter has limits on performance at high speeds because of the limitations of main rotor, such as compressibility issues on advancing side or… (more)

Subjects/Keywords: Rotorcraft; Redundant Controls; Optimization; Compound Helicopter; Flight Dynamics and Control; Performance

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APA (6th Edition):

Ozdemir, G. T. (2013). In-flight Performance Optimization for Rotorcraft with Redundant Controls. (Doctoral Dissertation). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/19980

Chicago Manual of Style (16th Edition):

Ozdemir, Gurbuz Taha. “In-flight Performance Optimization for Rotorcraft with Redundant Controls.” 2013. Doctoral Dissertation, Penn State University. Accessed September 19, 2019. https://etda.libraries.psu.edu/catalog/19980.

MLA Handbook (7th Edition):

Ozdemir, Gurbuz Taha. “In-flight Performance Optimization for Rotorcraft with Redundant Controls.” 2013. Web. 19 Sep 2019.

Vancouver:

Ozdemir GT. In-flight Performance Optimization for Rotorcraft with Redundant Controls. [Internet] [Doctoral dissertation]. Penn State University; 2013. [cited 2019 Sep 19]. Available from: https://etda.libraries.psu.edu/catalog/19980.

Council of Science Editors:

Ozdemir GT. In-flight Performance Optimization for Rotorcraft with Redundant Controls. [Doctoral Dissertation]. Penn State University; 2013. Available from: https://etda.libraries.psu.edu/catalog/19980

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