- About
-
The Global ETD Search service is a free service for researchers
to find electronic theses and dissertations. This service is
provided by the
Networked Digital Library of Theses and Dissertations.
Our metadata is collected from universities around the world. If you manage a university/consortium/country archive and want to be added, details can be found on the NDLTD website.
Search results
Showing 41 to 50 of 60 (0.291 seconds)Spelling suggestions: "subject:"dcotors (helicopters) -- aerodynamics"" "subject:"dcotors (helicopters) -- neurodynamics""
| 41 |
A method of computing the pressure distribution on a single-bladed hovering helicopter rotorShenoy, Koodige Rajarma 05 1900 (has links)
No description available.
|
| 42 |
Unsteady compressible lifting surface analysis for rotary wings using velocity potential modesKaladi, Vasudevan M. 08 1900 (has links)
No description available.
|
| 43 |
Solution procedure for the Navier-Stokes equations applied to rotorsWake, Brian E. 05 1900 (has links)
No description available.
|
| 44 |
Gust response and its alleviation for a hingeless helicopter rotor in cruising flight.Yasue, Masahiro January 1977 (has links)
Thesis. 1977. Ph.D.--Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. / MICROFICHE COPY AVAILABLE IN ARCHIVES AND AERONAUTICS. / Vita. / Includes bibliographical references. / Ph.D.
|
| 45 |
Aerodynamic shape optimization via control theory of helicopter rotor blades using a non-linear frequency domain approachTatossian, Charles A. January 2008 (has links)
No description available.
|
| 46 |
Effect of tip-speed ratio on induced velocities near a lifting rotorHeyson, Harry H. January 1958 (has links)
A theoretical investigation of the asymmetry of induced flow in the vicinity of a lifting rotor in forward flight has been conducted. The analysis is based upon an asymmetric wake which is a logical extension of that used for previous investigations. Equations for the induced velocities at an arbitrary point in space are presented in a form suitable for numerical integration. Numerical results for the normal induced velocity in the lateral plane of the rotor are presented in the form of tables and charts. Comparison with previously available measurements indicates an improvement in accuracy over older theories. The results should be useful in estimating the interference between wing and rotor of compound helicopters and convertiplanes. In addition the results should be applicable to the problem of mutual interference between rotors of multi-rotor helicopters. / Master of Science
|
| 47 |
Investigation of a stop-fold tiltrotorBosworth, Jeff. January 2009 (has links)
Thesis (M. S.)--Aerospace Engineering, Georgia Institute of Technology, 2010. / Committee Chair: Hodges, Dewey; Committee Member: Bauchau, Olivier; Committee Member: Sankar, Lakshmi. Part of the SMARTech Electronic Thesis and Dissertation Collection.
|
| 48 |
Aeroelastic optimization of a composite tilt rotorSoykasap, Omer 05 1900 (has links)
No description available.
|
| 49 |
Stability of elastically tailored rotor bladesFulton, Mark V. 05 1900 (has links)
No description available.
|
| 50 |
A preliminary design to include a stability and control study in hovering flight of a laterally disposed, single-bladed, counter-rotating, two-rotor helicopter with shrouded tail propellerEllis, William Roderick 12 1900 (has links)
No description available.
|
Page generated in 0.3085 seconds