Direct and Cross-Coupling Subsonic Moment Derivatives Due to Oscillatory Pitching and Yawing of an Aircraft-Like Model At Angles of Attack Up to 40 Degrees in Ames' 6' X 6' Wind Tunnel Laboratory Technical Report LTR-UA-38

Orlick-Ruckemann, K. J. & Hanff, E. S. & Laberge, J. G.

Published by National Research Council of Canada, Ottawa, 1976
Condition: Used - Very good Soft cover

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Used - Soft cover

Condition: Used - Very good

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