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Free-flight Experience of the Lateral Stability Characteristics at Low Lift of a 45° Swept-wing Rocket-propelled Model Equipped with a Nonlinear Yaw-rate Damper System at Mach Numbers from 0.76 to 1.73
Charles T. D'Aiutolo
William W. Willoughby
Lucille C. Coltrane
出版
National Advisory Committee for Aeronautics
, 1957
URL
http://books.google.com.hk/books?id=Mxu7ZwEACAAJ&hl=&source=gbs_api
