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THE ESTIMATION OF SHOCK PRESSURE RECOVERY AND EXTERNAL DRAG CONICAL CENTRE-BODY INTAKES AT SUPERSONIC SPEEDS.

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BookPublisher: Her Majesty'S Stationery Office, London 1959Description: 66.DDC classification: ARC | R&M 3035

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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	ARC R&M 3035 (Browse shelf)	Not for loan		TR11128

Total holds: 0

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Previous	ARC R&M 3029 MEASUREMENTS OF TWO-DIMENSIONAL DERIVATIVES ON A WING-AILERON-TAB SYSTEM WITH A 1541 SECTION AEROFOIL. PART II-DIRECT TAB AND CROSS AILERON-TAB DERIVATIVES.	ARC R&M 3032 THE EFFECTS OF TAPER ON THE SUPERVELOCITIES ON THREE-DIMENSIONAL WINGS AT ZERO INCIDENCE.	ARC R&M 3033 A SURVEY AND CORRELATION OF DATA ON HEAT TRANSFER BY FORCED CONVECTION AT SUPERSONIC SPEEDS.	ARC R&M 3035 THE ESTIMATION OF SHOCK PRESSURE RECOVERY AND EXTERNAL DRAG CONICAL CENTRE-BODY INTAKES AT SUPERSONIC SPEEDS.	ARC R&M 3036 A METHOD FOR CALCULATING THE PRESSURE DISTRIBUTION OVER JET-FLAPPED WINGS.	ARC R&M 3038 THE HARMONICALLY OSCILLATING WING WITH FINITE VORTEX TRAIL.	ARC R&M 3039 THE THEORETICAL DETERMINATION OF NORMAL MODES AND FREQUENCIES OF VIBRATION.	Next

Bound With Arc R&M3020-33,3036-39 Lack No.3022,3026,3028,3030-31,3034-37

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