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BOUNDARY-LAYER PREDICTION METHODS APPLIED TO COOLING PROBLEMS IN THE GAS TURBINE.

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BookPublisher: Her Majesty'S Stationery Office, London 1971Description: 19.DDC classification: ARC | C.P. 1164

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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. 1164 (Browse shelf)	Not for loan		TR11170

Total holds: 0

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Previous	ARC C.P. 1150 LIST OF CURRENT PAPERS PUBLISHED FOR THE AERONAUTICAL RESEARCH COUNCIL	ARC C.P. 1162 LOW- SPEED WIND-TUNNEL CALIBRATIONS OF THE PITOT AND STATIC PRESSURE SENSORS AND WIND VANES ON THE SHORT SC I AIRCRAFT.	ARC C.P. 1163 LOW-SPEED WIND-TUNNEL TESTS ON A FAMILY OF CAMBERED WINGS OF MILD GOTHIC PLANFORM OF ASPECT RATIO 1.4.	ARC C.P. 1164 BOUNDARY-LAYER PREDICTION METHODS APPLIED TO COOLING PROBLEMS IN THE GAS TURBINE.	ARC C.P. 1165 PILOTED SIMULATOR INVESTIGATIONS OF FLIGHT NEAR ZERO RATE OF CLIMB SPEED.	ARC C.P. 1166 SOME FULL-SCALE MEASUREMENTS OF THE FLOW IN THE WAKE OF A HANGAR.	ARC C.P. 1167 FLIGHT AND WIND-TUNNEL TESTS ON AN AERODYNAMICALLY COMPENSATED PILOT-STATIC HEAD FOR THE BAC 221 AIRCRAFT.	Next

Bound With Arc C.P. 1161-63, 1165-70.

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