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SUPERSONIC WIND-TUNNEL FLUTTER TESTS OF TWO RECTANGULAR WINGS

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BookPublisher: Her Majesty'S Stationery Office, London 1958Description: 15.DDC classification: ARC | R & M 3080

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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 3080 (Browse shelf)	Not for loan Untraceable		TR14425

Total holds: 0

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Previous	ARC R & M 3077 METHODS FOR DETERMINING THE WAVE DRAG OF NON-LIFTING WING-BODY COMBINATIONS	ARC R & M 3078 LOW-SPEED-TUNNEL MODEL TESTS ON THE FLOW STRUCTURE BEHIND A DELTA-WING AIRCRAFT AND A 4O DEG SWEPT-WING AIRCRAFT AT HIGH INCIDENCES	ARC R & M 3079 THE REPRESENTATION OF ENGINE AIRFLOW IN WIND-TUNNEL MODEL TESTING	ARC R & M 3080 SUPERSONIC WIND-TUNNEL FLUTTER TESTS OF TWO RECTANGULAR WINGS	ARC R & M 3106 Some visual observations of the effects of sweep on the low-speed flow over a sharp-edged plate at incidence	ARC R & M 3107 Experimental study of surface flow and part-span vortex layers on a cropped arrowhead wing	ARC R & M 3108 Some effects of shock-induced separation of turbulent boundary layers in transonic flow past aerofoils	Next

Bound With Arc R & M 3070-3079,Lack No. 3075

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