Global ETD Search

111	Stability of elastically tailored rotor blades Fulton, Mark V. 05 1900 (has links) No description available. Fluid dynamics Mathematical models Rotors (Helicopters) Rotors (Helicopters) Aerodynamics
112	Study of a low-dispersion finite volume scheme in rotocraft noise prediction Wang, Gang 05 1900 (has links) No description available. Rotors (Helicopters) Noise Helicopters Noise Aerodynamic noise Mathematical models
113	Optimal helicopter trajectory planning for terrain following flight Kim, Eulgon 12 1900 (has links) No description available. Helicopters Control systems Helicopters Flight testing Control theory
114	Dynamic stability analysis of helicopter blade with adaptive damper / Morozova, Natalia, January 1900 (has links) Thesis (M.App.Sc.) - Carleton University, 2003. / Includes bibliographical references (p. 131-133). Also available in electronic format on the Internet.
115	Modelling and stability analysis of a composite helicopter rotor blade with integrated active fibres / Saxton, Caroline R. January 1900 (has links) Thesis (M. App. Sc.)--Carleton University, 2003. / Includes bibliographical references (p. 118-124). Also available in electronic format on the Internet.
116	A multi-fidelity framework for physics based rotor blade simulation and optimization Collins, Kyle Brian. January 2008 (has links) Thesis (Ph.D)--Aerospace Engineering, Georgia Institute of Technology, 2009. / Committee Co-Chair: Dr. Dimitri Mavris; Committee Co-Chair: Dr. Lakshmi N. Sankar; Committee Member: Dr. Daniel P. Schrage; Committee Member: Dr. Kenneth S. Brentner; Committee Member: Dr. Mark Costello. Part of the SMARTech Electronic Thesis and Dissertation Collection.
117	Modeling helicopter dynamic loads using artificial neural networks / Nosek, Michael, January 1993 (has links) Thesis (M.S.)--Virginia Polytechnic Institute and State University, 1993. / Vita. Abstract. Includes bibliographical references (leaves 89-90). Also available via the Internet.
118	Variable geometric performance for rotary wing aircraft Adams, George Francis January 1980 (has links) With the advent of variable geometric wing surfaces providing noticeable performance improvements in fixed wing aircraft, a theoretical study of the performance advantages of variable geometry designs for rotary wing aircraft is presented. The analysis is developed in three sections, namely: 1) Theoretical justification of variable geometry through application of simple blade element equations; 2) A simplified design proposal to implement variable geometry in rotor systems; and 3) A numerical comparison of fixed and variable geometry performance statistics applied to specifications of an actual helicopter. / Master of Engineering LD5655.V851 1980.A325 Rotors (Helicopters) Helicopters -- Design and construction
119	Pressure measurements near the tip of a hovering model rotor blade and a preliminary investigation of the flow in the rotor wake Shivananda, Tumkur Parameswaraiah 12 1900 (has links) No description available. Rotors (Helicopters) Aerodynamics Wakes (Aerodynamics)
120	Effect of compressibility on three-dimensional helicopter rotor blade flutter White, William Felton 05 1900 (has links) No description available. Flutter (Aerodynamics) Compressibility Rotors (Helicopters)

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