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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

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BookPublisher: Her Majesty'S Stationery Office, London 1970Description: 21.DDC classification: ARC | C.P. 1108

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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. 1108 (Browse shelf)	Not for loan Untraceable		A13862

Total holds: 0

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Previous	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	ARC C.P. 1110 THE ESTIMATION OF THE LOADING ON SWEPT WINGS WITH EXTENDING CHORD FLAPS AT SUBSONIC SPEEDS	ARC C.P. 1111 INTERIM NOTE ON TESTS WITH A WING-MOUNTED FAN NACELLE WITH THE FAN JET SIMULATED BY COLD AIR BLOWING AND ALTERNATIVELLY BY A GAS GENERATOR SHROUD	Next

Bound With Arc C.P.1100-1107,1109-1110 Lack No.1104

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