- About
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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 31 to 40 of 290 (0.065 seconds)Spelling suggestions: "subject:"helicopter""
| 31 |
The effect of wake dynamics on rotor eigenvalues in forward flightWang, Yi-Ren 05 1900 (has links)
No description available.
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| 32 |
Towards a unified analysis methodology for composite rotor bladesAtilgan, Ali Rana 08 1900 (has links)
No description available.
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| 33 |
Design of a helicopter automatic flight control system using adaptive controlFitzsimons, Philip Matthew 08 1900 (has links)
No description available.
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| 34 |
Application of a state-space wake model to a servo flap controlled rotor in hoverStettner, Martin 12 1900 (has links)
No description available.
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| 35 |
Trailing edge flap control of dynamic stall on helicopter rotor blades /Davis, Gregory Lloyd. January 1900 (has links)
Thesis (M.App.Sc.) - Carleton University, 2006. / Includes bibliographical references (p. 153-158). Also available in electronic format on the Internet.
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| 36 |
A 3D Theodorsen-based rotor blade flutter model using normal modes /Rauchenstein, Werner J. January 2002 (has links) (PDF)
Thesis (M.S. in Aeronautical Engineering)--Naval Postgraduate School, September 2002. / Thesis advisor(s): E. Roberts Wood, Mark A. Couch. Includes bibliographical references (p. 55-56). Also available online.
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| 37 |
The computation of aerodynamic loads on helicopter blades in forward flight, using the method of the accelerationpotential.Holten, Th. van. January 1900 (has links)
Thesis - Technische hogeschool Delft. / Bibliography: p. 108.
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| 38 |
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.
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| 39 |
A multidisciplinary design approach to size stopped rotor/wing configurations using reaction drive and circulation controlTai, Jimmy C. M. 08 1900 (has links)
No description available.
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| 40 |
An experimental and theoretical study of helicopter rotor noise.Lee, Ying-Chieh Albert January 1975 (has links)
Thesis. 1975. Ph.D.--Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. / Vita. / Includes bibliographical references. / Ph.D.
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