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WIND TUNNEL TESTS ON A RECTANGULAR, TWIN DUCT, VARIABLE GEOMETRY AIR INTAKE AT SUPERSONIC SPEEDS.

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BookPublisher: Her Majesty'S Stationery Office, London 1966Description: 52.DDC classification: ARC | C.P. 944

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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. 944 (Browse shelf)	Not for loan		TR10706

Total holds: 0

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Previous	ARC C.P. 940 PROJECT TOPCAT	ARC C.P. 942 AN EXPERIMENTAL INVESTIGATION OF THE TWO-DIMENSIONAL WALL JET.	ARC C.P. 943 A THEORITICAL INVESTIGATION OF THE EFFECT OF ASPECT RATIO ON AXIAL FLOW COMPRESSOR PERFORMANCE.	ARC C.P. 944 WIND TUNNEL TESTS ON A RECTANGULAR, TWIN DUCT, VARIABLE GEOMETRY AIR INTAKE AT SUPERSONIC SPEEDS.	ARC C.P. 945 A CONVENIENT REPRESENTATION OF CREEP STRAIN DATA FOR PROBLEMS INVOLVING TIME-VARYING STRESSES AND TEMPERATURES.	ARC C.P. 946 AN ANALOGUE COMPUTER FOR ON-LINE CORRECTION OF WIND TUNNEL FORCE AND MOMENT DATA.	ARC C.P. 947 A NOTE ON THE DESIGN AND CONTRUCTION OF A LOW A LOW-PRESSURE CALIBRATOR AND A COMPARISON WITH SHOCK-TUBE AND STATIC CALIBRATION METHODS.	Next

Bound With Arc C.P.941-43, 945-50

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