- 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 1 to 10 of 25 (0.061 seconds)Spelling suggestions: "subject:"dictability off airplanes."" "subject:"dictability oof airplanes.""
| 1 |
Aeroservoelastic stability analysis of an airplane with a control augmentation system /Moore, Robert Lee, January 1978 (has links)
Thesis (Ph. D.)--Ohio State University, 1978. / Includes vita. Includes bibliographical references (leaves 175-177). Available online via OhioLINK's ETD Center.
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| 2 |
THEORETICAL INVESTIGATION AND OPTIMIZATION OF AN AIRPLANE GUST ALLEVIATION SYSTEMPolve, James Herschal, 1921- January 1966 (has links)
No description available.
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| 3 |
Gust alleviation in aircraft using forward mounted control surfacesTherrien, Francois Xavier, 1928- January 1962 (has links)
No description available.
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| 4 |
An investigation of the directional and lateral stick-fixed stabilities of the canard with end plate vertical tail surfacesKenner, Lewis Morton 05 1900 (has links)
No description available.
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| 5 |
Additional moments of inertia of a full-scale airplane and its effects on dynamic lateral stabilityLucas, Robert Earl 12 1900 (has links)
No description available.
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| 6 |
A simulation model of atmospheric turbulence for rotorcraft applicationsRiaz, Jamshed 05 1900 (has links)
No description available.
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| 7 |
Flight test investigation of propeller effects on the static longitudinal stability of the E-2C airplaneJamison, Glenn Richard, January 2006 (has links) (PDF)
Thesis (M.S.) -- University of Tennessee, Knoxville, 2006. / Title from title page screen (viewed on Sept. 14, 2006). Thesis advisor: U. P. Solies. Vita. Includes bibliographical references.
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| 8 |
Aeroservoelastic stability analysis of an airplane with a control augmentation system /Moore, Robert Lee January 1978 (has links)
No description available.
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| 9 |
Theory, design and experimental study of an eddy-current/hydromechanical stability augmentor for aircraft /Jenney, Gavin D. January 1979 (has links)
No description available.
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| 10 |
Finite-state inflow applied to aeroelastic flutter or fixed and rotating wingsNibbelink, Bruce D. 05 1900 (has links)
No description available.
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