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TESTS AT A MACH NUMBER OF 2.0 ON A RECTANGULAR, TWIN-DUCT AIR INTAKE WITH VARIABLE GEOMETRY,SITUATED IN THE FLOW FIELD OF A SLENDER WING

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BookPublisher: Her Majesty'S Stationery Office, London 1970Description: 14.DDC classification: ARC | C.P. 1122

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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 C.P. 1122 (Browse shelf)	Not for loan		TR13875

Total holds: 0

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Previous	ARC C.P. 1101 NORMAL SHOCK-WAVE TABLES FOR AIR, ARGON, CARBON DIOXIDE, CARBON MONOXIDE, HYDROGEN, NITROGEN, NITROUS OXIDE AND OXYGEN	ARC C.P. 1102 PRELIMINARY FLIGHT ASSESSMENT OF THE LOW-SPEED HANDLING OF THE BAC 221 OGEE-WING RESEARCH AIRCRAFT	ARC C.P. 1117 AN INVESTIGATION OF THE STRESSES IN A WIND TUNNEL CORNER SECTION	ARC C.P. 1122 TESTS AT A MACH NUMBER OF 2.0 ON A RECTANGULAR, TWIN-DUCT AIR INTAKE WITH VARIABLE GEOMETRY,SITUATED IN THE FLOW FIELD OF A SLENDER WING	ARC C.P. 1126 THE ROLE OF HEAT CONDUCTION IN LEADING EDGE HEATING THEORY AND EXPERIMENT	ARC C.P. 1127 LIQUID AND VAPOUR COOLING SYSTEMS FOR GAS TURBINES	ARC C.P. 1130 EXPERIMENTAL INVESTIGATION OF THE EFFECT OF TRAILING-EDGE SWEEPBACK ON THE SUBSONIC LONGITUDINAL CHARACTERISTICS OF SLENDER WINGS	Next

Bound With Arc C.P.1121,1123-30

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