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A PRELIMENTAL INVESTIGATION OF SHOCK-WAVE DEVELOPMENT ON AEROFOILES.

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BookPublisher: Her Majesty'S Stationery Office, London 1966Description: 10.DDC classification: ARC | C.P 964

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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 964 (Browse shelf)	Not for loan Untraceable		TR14434

Total holds: 0

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Previous	ARC C.P 922 INVESTIGATION OF THE NORMAL FORCE CHARACTERISTICS OF SLENDER DELTA WINGS WITH VARIOUS RHOMBIC CROSS-SECTIONS IN SUBSONIC CONICAL FLOW	ARC C.P 962 THE EFFECT OF BLEED ON THE PRESSURE OF SEVERAL SHROUDED AND UNSHROUDED PROPELLING NOZZLES AT M=1.96.	ARC C.P 963 THE CALCILATION OF MOMENTUM THICKNESS IN A TURBULENT BOUNDARY LAYER AT MACH NUMBERS UP TO UNITY.	ARC C.P 964 A PRELIMENTAL INVESTIGATION OF SHOCK-WAVE DEVELOPMENT ON AEROFOILES.	ARC C.P 965 HEAT YRANSFER IN THE VICINITY OF A 15 DEGREE COMPRESSION CORNER AT MACH NUBMERS FROM 2.5 TO 4.4.	ARC C.P 966 SOME FURTHER NOTES ON THE LAMINAR BOUNDARY LAYER DEVELOPMENT AND RUNNING TIME IN A SHOCK TUBE.	ARC C.P 967 THE DISTRIBUTION OF A WALL PRESSURE RISE IN A TURBULENT BOUNDARY LAYER.	Next

Bound With Arc C.P-961-963,965-970.

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