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ON THE INTERACTION OF THE TRANSMITTED SHOCK WITH THE BOUNDARY LAYER IN A SHOCK TUBE USING ARGON AS A TEST GAS.

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BookPublisher: Her Majesty'S Stationery Office, London 1967Description: 9.DDC classification: ARC | C.P. 879

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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. 879 (Browse shelf)	Not for loan Untraceable		TR11012

Total holds: 0

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Previous	ARC C.P. 876 CHARACTERISTICS OF HIGH-SPEED WIND TUNNEL IN THE UNITED KINGDOM RELEVANT TO AEROELASTIC-MODEL TESTS.	ARC C.P. 877 THE FLAPPING BEHAVIOUR OF A HELICOPTER ROTOR AT HIGH TIP-SPEED RATIOS.	ARC C.P. 878 COMPARISION OF HELICOPTER AND AEROPLANE VERTICAL ACCELERATIONS IN TURBULENCE.	ARC C.P. 879 ON THE INTERACTION OF THE TRANSMITTED SHOCK WITH THE BOUNDARY LAYER IN A SHOCK TUBE USING ARGON AS A TEST GAS.	ARC C.P. 881 THE INTERACTION OF THE REFLECTED SHOCK WITH THE BOUNDARY LAYER IN A SHOCK TUBE AND ITS INFLUANCE ON THE DURATION OF HOT FLOW IN THE REFLECTED-SHOCK TUNNEL. PART-1	ARC C.P. 882 BULK COMPRESSIBILITY EFFECTS IN THE R.A.R.D.E.NO.3 HYPERSONIC GUN TUNNEL.	ARC C.P. 883 A STUDY ON THE RUNNING TIMES IN REFLECTED SHOCK TUNNEL.	Next

Bound With Arc C.P.869-78

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