The dynamic stability derivatives of a slender wing at zero and moderate lift : a comparison of theory with free-flight model tests, M = 0.8 to 2.0 /

Bibliographic Details
Main Authors:	Ross, A. Jean (Author), Edwards, Geraldine F. (Author), Waterfall, A. P. (Author)
Format:	Book
Language:	English
Published:	London : Her Majesty's Stationery Office, 1975.
Series:	Current papers (Aeronautical Research Council (Great Britain)) ; no. 1310.
Subjects:	Airplanes > Wings, Triangular. Stability of airplanes. Lift (Aerodynamics) Avions > Ailes delta. Avions > Stabilité. Portance. Airplanes > Wings, Triangular Stability of airplanes Technical reports.

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