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Ames Research Center
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Bousman, William G.
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1
Integrated Technology Rotor Methodology Assessment Workshop : proceedings of a workshop.
Published 1988
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2
A comparison of lifting-line and CFD methods with flight test data from a research puma helicopter.
Published 1996
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Aerodynamic limitations of the UH-60A rotor /
by
Coleman, Colin P.
Published 1996
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An examination of the aerodynamic moment on rotor blade tips using flight test data and analysis.
by
Maier, Thomas H.
Published 1993
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Estimation of blade airloads from rotoer blade bending moments /
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Bousman, William G.
Published 1987
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Correlation of Puma airloads : lifting-line and wake calculation /
Published 1989
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The effects of structural flap-lag and pitch-lag coupling on soft inplane hingeless rotor stability in hover /
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Bousman, William G.
Published 1990
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Airfoil dynamic stall and rotorcraft maneuverability /
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Bousman, William G.
Published 2000
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Ames Research Center
Bousman, William G.
United States. Army Aviation Research and Technology Activity
4 results
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Coleman, Colin P.
1 results
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Integrated Technology Rotor Methodology Assessment Workshop Ames Research Center
1 results
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Maier, Thomas H.
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McNulty, Michael J.
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U.S. Army Aviation and Troop Command
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United States. Army
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United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch
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