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ON THE DEVELOPMENT OF THE INCOMPRESSIBLE TURBULENT BOUNDARY LAYER

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BookPublisher: Her Majesty'S Stationery Office, London 1967Description: 47.DDC classification: ARC | R&M 3484

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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 3484 (Browse shelf)	Not for loan Untraceable		TR14475

Total holds: 0

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Previous	ARC-R&M 3480 TRANSONIC FLOW IN THE THROAT REGION OF AN ANNULAR NOZZLE WITH AN ARBITRARY SMOOTH PROFIL.	ARC R&M 3482 FLIGHT DETERMINATION OF WING FLOW PATTERNS AND BUFFET BOUNDARIES FOR THE FAIREY DELTA 2 AIRCRAFT AT MACH NUMBERS BETWEEN 0.4 AND 1.3, AND COMPARISON WITH WIND TUNNEL RESULTS	ARC R&M 3483 LEAKAGE AND SECONDARY FLOWS IN COMPRESSOR CASCADES	ARC R&M 3484 ON THE DEVELOPMENT OF THE INCOMPRESSIBLE TURBULENT BOUNDARY LAYER	ARC R&M 3485 FLIGHT MEASUREMENTS OF THE ELEVATOR AND AILERON HINGE-MOMENT DERIVATIVES OF THE FAIREY DELTA 2 AIRCRAFT UP TO A MACH NUMBER OF 1.6 AND COM-PARISONS WITH WIND-TUNNEL RESULTS	ARC R&M 3486 LOW-SPEED WIND-TUNNEL TESTS ON A 1/8TH SCALE MODEL OF THE HANDLEY-PAGE HP.115	ARC R&M 3487 THE CALCULATION OF THE SPANWISE LOADING OF SWEPTBACK WINGS WITH FLAPS OR ALL-MOVING TIPS AT SUBSONIC SPEEDS	Next

Bound With Arc R&M 3481-3483,3485-3490

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