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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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THEORETICAL INVESTIGATION AND OPTIMIZATION OF AN AIRPLANE GUST ALLEVIATION SYSTEMPolve, James Herschal, 1921- January 1966 (has links)
No description available.
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Gust alleviation in aircraft using forward mounted control surfacesTherrien, Francois Xavier, 1928- January 1962 (has links)
No description available.
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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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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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A simulation model of atmospheric turbulence for rotorcraft applicationsRiaz, Jamshed 05 1900 (has links)
No description available.
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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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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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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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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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