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CALCULATIONS OF THE FLOW OVER THICK,CONICAL,SLENDER WINGS WITH LEADING-EDGE SEPARATION

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BookPublisher: Her Majesty'S Stationery Office, London 1972Description: 66.DDC classification: ARC | R&M 3694

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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 3694 (Browse shelf)	Not for loan Untraceable		TR16975

Total holds: 0

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Previous	ARC R&M 3688 AN INVESTIGATION OF ANNULAR AEROFOILS FOR TURBOFAN ENGINE COWLS	ARC R&M 3689 THE MEASUREMENT OF GROUND EFFECT USING A FIXED GROUND BOARD IN A WIND TUNNEL	ARC R&M 3693 PRESSURE MEASUREMENTS ON A MODEL DELTA WING UNDERGOING OSCILLATORY DEFORMATION	ARC R&M 3694 CALCULATIONS OF THE FLOW OVER THICK,CONICAL,SLENDER WINGS WITH LEADING-EDGE SEPARATION	ARC R&M 3695 THE VORTEX DRAG OF A SWEPT WING WITH PART-SPAN FLAPS	ARC R&M 3696 EXPERIMENTS IN TURBULENT BOUNDARY LAYERS WITH FOREIGN GAS INJECTION	ARC R&M 3698 THE EFFECTS OF RIDGE EXCRESCENCES AND TRAILING-EDGE CONTROL GAPS ON TWODIMENSIONAL AEROFOIL CHARACTERISTICS	Next

Bound With Arc R&M 3692-3693, 3695-3699, Lack No. 3697

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