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An investigation of the flow about a plane half-wing of cropped-delta planform and 6 per cent symmetrical section at stream mach numbers between 0.8 and 1.41

By: E W.E Rogers.

Contributor(s): C J Berry.

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BookPublisher: DDC classification: ARC | R&M 3286

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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 3286 (Browse shelf)	Not for loan Untraceable		TR16764

Total holds: 0

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Previous	ARC R&M 3283 On the flexure of thin built-up wings	ARC R&M 3284 Flutter of an all-moving tailplane	ARC R&M 3285 Seaplane impact - a review of theoretical and experimental results	ARC R&M 3286 An investigation of the flow about a plane half-wing of cropped-delta planform and 6 per cent symmetrical section at stream mach numbers between 0.8 and 1.41	ARC R&M 3287 Comparision of results in the A.R.E. transonic tunnel on a small and a large model of a slender wing	ARC R&M 3288 Experiments on a delta wing with jet-assisted lift	ARC R&M 3289 USE OF CONICAL CAMBER TO PRODUCE FLOW ATTACHMENT AT THE LEADING EDGE OF A DELTA WING AND TO MINIMIZE LIFT-DEPENDENT DRAG AT SONIC AND SUPERSONIC SPEEDS	Next

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