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Dynamic stall characteristics of an oscillating airfoil in a harmonically varying freestream velocityMalone, John Bruce 12 1900 (has links)
No description available.
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Inverse methodology for multi-point aerodynamic rotor blade designTapia, Fidencio 05 1900 (has links)
No description available.
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Identification of an improved body aerodynamics model for the BO 105Bitzer, Michael 12 1900 (has links)
No description available.
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Military innovation and the helicopter a comparison of development in the United States army and marine corps, 1945-1965 /Horn, Carl John, January 2003 (has links)
Thesis (Ph. D.)--Ohio State University, 2003. / Title from first page of PDF file. Document formatted into pages; contains vi, 356 p. Includes bibliographical references (p. 341-356). Available online via OhioLINK's ETD Center
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Application of frequency-domain-method to rotorcraft aerodynamicsKumar, Manish. January 2008 (has links)
Thesis (Ph.D.)--Syracuse University, 2008. / "Publication number: AAT 3333572."
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Vision-based control and flight optimization of a rotorcraft UAV / /Hubbard, David Christian, January 2007 (has links) (PDF)
Thesis (M.S.)--Brigham Young University. Dept. of Computer Science, 2007. / Includes bibliographical references (p. 79-81).
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Trajectory optimization for helicopter Unmanned Aerial Vehicles (UAVs)Gatzke, Benjamin Thomas. January 2010 (has links) (PDF)
Thesis (M.S. in Applied Mathematics)--Naval Postgraduate School, June 2010. / Thesis Advisor(s): Kang, Wei ; Second Reader: Zhou, Hong. "June 2010." Description based on title screen as viewed on July 14, 2010. Author(s) subject terms: Nonlinear model, trajectory optimization, state and control variables, cost function Includes bibliographical references (p. 59-60). Also available in print.
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Study of the electrostatic field and charge distribution in a vortex seeded with dust /Daugherty, John William January 1973 (has links)
No description available.
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Development and validation of a tire model for a real time simulation of a helicopter tranversing and manoeuvring on a ship flight deck /Tremblay, Jason January 1900 (has links)
Thesis (M.App.Sc.) - Carleton University, 2007. / Includes bibliographical references (p. 108-112). Also available in electronic format on the Internet.
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Full state control of a Fury X-Cell unmanned helicopterVan Schalkwyk, Carlo 03 1900 (has links)
Thesis (MScEng (Electrical and Electronic Engineering))--University of Stellenbosch, 2009. / This thesis describes the successful development of an autopilot for an unmanned
radio controlled helicopter. It presents a non-linear helicopter model. An adaptive
linearised model is derived and used to design a controller. The adaptive full
state controller is tested in various ways, including two aerobatic manoeuvres. A
number of analyses are performed on the controller, including its robustness to parameter
changes, noisy estimates, wind and processing power. The controller is
compared with a non-adaptive counterpart, which leads to the conception, design
and analysis of a much improved control structure. Practical flight test results are
presented and analysed.
In some instances available literature was reworked and re-derived to produce
a genericmodel-controller package that can easily be adapted for helicopters of any
make, model and size.
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