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Dynamic stability derivatives of a twin-jet fighter model for angles of attack from -10 ̊to 110
Sue B. Grafton and Charles E. Libbey.

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Main Author: Grafton, Sue B.
Related Names: Libbey, Charles E.
Language(s): English
Published: Washington, D.C. : National Aeronautics and Space Administration ; 1971.
Subjects: Fighter planes > Fighter planes / Aerodynamics.
Spin (Aerodynamics)
Angle of attack (Aerodynamics)
Airplanes > Airplanes / Wings, Swept-back > Airplanes / Wings, Swept-back / Aerodynamics.
Physical Description: 36 p. : ill. ; 27 cm.
Locate a Print Version: Find in a library

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Full view University of Illinois at Urbana-Champaign
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