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THE DISTRIBUTION OF A WALL PRESSURE RISE IN A TURBULENT BOUNDARY LAYER.

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BookPublisher: Her Majesty'S Stationery Office, London 1966Description: 21.DDC classification: ARC | C.P 967

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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 967 (Browse shelf)	Not for loan		TR14437

Total holds: 0

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Previous	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.	ARC C.P 968 THE DRAG OF SOME WEDGE CENTRE-BODY INTAKES AT MACH NUMBERS OF 1.56,1.86 AND 2.14.	ARC C.P 969 AN INVSTIGATION INTO A TECHNIQUE FOR MEASURE JET INTERFERENCE EFFECTS USING FREE-FLIGHT MODELS.	ARC C.P 970 TECHNIQUES FOR TESTS ON STRUCTURES SUBJECT TO KINETIC HEATING.	Next

Bound With Arc Cp-961-966.968-970.

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