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Calculation of the effects of blowing from the leading edges of a cambered delta wing

By: E. J. Barsby.

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BookPublisher: DDC classification: TR | R & M-3800

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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	TR R & M-3800 (Browse shelf)	Not for loan		A58429

Total holds: 0

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Previous	TR R & M 3744 Low-speed wind tunnel measurements of the lift,drag and pitching moment of a series of cropped delta wings	TR R & M-1730 Flight of a helicopter	TR R & M-2549 Example in wing theory at supersonic speed	TR R & M-3800 Calculation of the effects of blowing from the leading edges of a cambered delta wing	TR R & M-3804 Theoretical determination of subsonic oscillatary airfarce coefficients	TR R & M-3805 Vortex breakdown-some obser-vations in flight on the HP115 aircraft	TR R & M-3806 Measurements of control-surface oscillatary derivatives on a & wept-back,tapered model wing in two transonic tunnels	Next

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