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Theoretical investigation of the longitudinal response characteristics of a swept-wing fighter airplane having a pitch-attitude control system

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BookPublisher: Washington, D. C. National Advisory Committee for Aeronautics 1953Description: 41p.DDC classification: NACA | TN-2882

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Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	Reference	NACA TN-2882 (Browse shelf)	Not for loan		67708B

Total holds: 0

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