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THEORETICAL PRESSURE DISTRIBUTIONS ON FOUR SIMPLE WING SHAPES FOR A RANGE OF SUPERSONIC FLOW CONDITONS

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BookPublisher: Her Majesty'S Stationery Office, London 1971Description: 9.DDC classification: ARC | C.P. 1178

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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. 1178 (Browse shelf)	Not for loan		TR14161

Total holds: 0

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Previous	ARC C.P. 1174 AN IMPROVED TECHNIQUE OF STABILITY TESTING IN FREE FLIGHT AT TRANSONIC SPEEDS, APPLIED TO A NON-LIFTING SLENDER WING	ARC C.P. 1175 PITOT-STEM BLOCKAGE CORRECTIONS IN UNIFORM AND NON-UNIFORM FLOW	ARC C.P. 1177 AIR CONDENSATION EFFECTS AT M=8.5 MEASURED ON THE DRAG AND THE WAKE OF A MAGNETICALLY SUSPENDED 20 DEG. CONE	ARC C.P. 1178 THEORETICAL PRESSURE DISTRIBUTIONS ON FOUR SIMPLE WING SHAPES FOR A RANGE OF SUPERSONIC FLOW CONDITONS	ARC C.P. 1179 THE PERFORMANCE OF AXIAL-FLOW COMPRESSORS OF DIFFERING BLADE ASPECT RATIO	ARC C.P. 1180 A SYSTEMATIC APPROACH TO THE DESIGN OF RADIAL INFLOW AND MIXED FLOW TURBINES	ARC C.P. 1193 CURVATURE EFFECTS IN THE DIFFRACTION OF SHORT WAVES INTO A SHADOW	Next

Bound With Arc C.P. 1171-1177,1179-1180

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