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THE RESPONSE OF A CONSTANT-PRESSURE TURBULENT BOUNDARY LAYER TO THE SUDDEN APPLICATION OF AN ADVERSE PRESSURE GRADIENT

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BookPublisher: Her Majesty'S Stationery Office, London 1969Description: 30.DDC classification: ARC | R&M 3575

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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 R&M 3575 (Browse shelf)	Not for loan		TR17013

Total holds: 0

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Previous	ARC R&M 3571 LOW-SPEED WIND-TUNNEL TESTS ON THE EFFECTS OF TAIPLANE AND NACELLE POSITION ON THE SUPERSTALL CHARACTERISTICS OF TRANSPORT AIRCRAFT	ARC R&M 3572 THE SUBERITICAL RESPONSE AND FLUTTER OF A SLENDER WING MODEL AIRCRAFT	ARC R&M 3574 HEAT TRANSFER AND TRANSITION MEASUREMENTS AT M=8.5 ON A DELTA MODEL AND A FLAT PLATE AT INCIDENCE	ARC R&M 3575 THE RESPONSE OF A CONSTANT-PRESSURE TURBULENT BOUNDARY LAYER TO THE SUDDEN APPLICATION OF AN ADVERSE PRESSURE GRADIENT	ARC R&M 3576 A MOMENTUM ANALYSIS OF LIFTING SURFACES IN INVISCID SUPERSONIC FLOW	ARC R&M 3577 FLIGHT MEASUREMENTS OF THE LIFT, LONGITUDINAL TRIM AND DRAG OF THE FAIREY DELTA 2 AT MACH NUMBERS UP TO 1.65 AND COMPARISONS WITH WIND-TUNNEL RESULTS	ARC R&M 3578 SOME INVESTIGATIONS INTO THE SPANWISE NON-UNIFORMITY OF NOMINALLY TWO-DIMENSIONAL INCOM-PRESSIBLE BOUNDARY LAYERS DOWNSTREAM OF GAUZE SCREENS	Next

Bound With Arc R&M 3570-3574, 3576-3579, Lack No. 3573

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