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A WIND-TUNNEL INVESTIGATION OF THE STALLING PERFORMANCE OF TWO COMPRESSOR CASCADES OF DIFFERENT ASPECT RATIOS AT LOW SPEED

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BookPublisher: Her Majesty'S Stationery Office, London 1970Description: 12.DDC classification: ARC | C.P. 1103

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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. 1103 (Browse shelf)	Not for loan Untraceable		A13858

Total holds: 0

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Previous	ARC C.P. 1100 LIST OF CURRENT PAPERS NUMBERS 1051-1100	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. 1103 A WIND-TUNNEL INVESTIGATION OF THE STALLING PERFORMANCE OF TWO COMPRESSOR CASCADES OF DIFFERENT ASPECT RATIOS AT LOW SPEED	ARC C.P. 1105 LOW SPEED FLIGHT TESTS ON A TAILLESS DELTA WING AIRCRAFT (AVRO 707B)	ARC C.P. 1108 LOW SPEED WIND-TUNNEL TESTS ON AN UNSWEPT WING-FUSELAGE MODEL OF ASPECT RATIO 9.8, WITH TANGENTIAL BLOWING OVER TRAILING-EDGE FLAPS AND AILERONS, INCLUDING THE EFFECT OF SLIPSTREAM	ARC C.P. 1109 INFLUENCE OF WING ROOT SHAPING ON THE PRESSURE DISTRIBUTION OF SWEPT-WING BODY CONFIGURATIONS	Next

Bound With Arc C.P.1100-1102,1105-1110 Lack No.1104

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