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CALCULATION OF THE VELOCITY DISTRIBUTION DUE TO THICKNESS FOR SWEPT WINGS WITH SUBSONIC EDGES AT SUPERSONIC SPEEDS

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BookPublisher: Her Majesty'S Stationery Office,London 1964Description: 38.DDC classification: HMSO-R&M-654 | -

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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	HMSO-R&M-654 - (Browse shelf)	Not for loan		TR9027

Total holds: 0

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Previous	HMSO-R&M-3380 - SOME TESTS ON HIGH-REACTION COMPRESSOR BLADING	HMSO-R&M-652 - STATIC AND DYNAMICS RESPONSE PROPERTIES OF INCIDENCE VANES WITH AERODYNAMIC AND INTERNAL VISCOUS DAMPING	HMSO-R&M-653 - FLIGHT MEASUREMENTS OF THE DUTCH ROLL CHARACTERISTICS OF A 60 DEGREE DELTA WING AIRCRAFT (FAIREY DELTA 2) AT MACH NUMBERS FROM 0.4 TO 1.5 WITH STABILITY DERIVATIVES EXTRACTED BY VECTOR ANALYSIS	HMSO-R&M-654 - CALCULATION OF THE VELOCITY DISTRIBUTION DUE TO THICKNESS FOR SWEPT WINGS WITH SUBSONIC EDGES AT SUPERSONIC SPEEDS	HMSO-R&M-655 - PROPAGATION OF FATIGUE CRACKS IN WIDE UNSTIFFENED ALUMINIUM ALLOY SHEETS	HMSO-R&M-656 - 8FT. X 6FT. TRANSONIC WIND TUNNEL TESTS ON A 1/24 SCALE MODEL OF THE FAIREY DELTA 2 (ER.103)	HMSO-R&M-657 - PRESSURE MEASUREMENTS ON A CONE-CYLINDER-FLARE CONFIGURATION AT M=6.85 AND INCIDENCE UP TO 30/CIRC	Next

Bound With Hmso-R&M-651-60

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