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NASA TN [D-6090] : DYNAMIC STABILITY DERIVATIVES OF A TWIN-JET FIGHTER MODEL FOR ANGLES OF ATTACK FROM -10(DEGREE) TO 110(DEGREE)

Series: NASA Technical Note. Publisher: Nasa, Washington, D.C. 1971Description: 36.Subject(s): Aerodynamics

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Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	General Stacks	NASA TN D-6091 - (Browse shelf)	Not for loan		TR9515

Total holds: 0

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NASA Technical Note D-6090-99
Bounded Volumes Accession No. 101225; Contents: TR9515-22

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