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A STUDY OF THE EFFECT OF LEADING-EDGE MODIFICATIONS ON THE FLOW OVER A 50-DEG SWEPTBACK WING AT TRANSONIC SPEEDS

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BookPublisher: Her Majesty'S Stationery Office, London 1962Description: 80.DDC classification: ARC | R&M 3270

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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 3270 (Browse shelf)	Not for loan Untraceable		TR17109

Total holds: 0

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Previous	ARC R&M 3266 STRESSE PRODUCED IN AN INFINITE ELASTIC PLATE BY THE APPLICATION OF LOADS TRAVELLING WITH UNIFORM VELOCITY ALONG THE BOUNDING SURFACES	ARC R&M 3267 THE EFFECT OF TEMPERATURE VARIATIONS IN THE PLANE AND THROUGH THE THICKNESS OF A CIRCULAR LENTICULAR PLATE	ARC R&M 3268 EFFECTS OF WING STIFFNESS AND INERTIA CHANGES ON THE MODES AND FREQUENCIES OF A MODEL DELTA AIRCRAFT	ARC R&M 3270 A STUDY OF THE EFFECT OF LEADING-EDGE MODIFICATIONS ON THE FLOW OVER A 50-DEG SWEPTBACK WING AT TRANSONIC SPEEDS	ARC R&M 3272 Theoretical investigation of the longitudinal stability, control and response characteristics of jet-flap aircraft	ARC R&M 3273 Performance of supersonic turbine nozzles	ARC R&M 3274 Free-flight measurements of the transonic roll-damping characteristics of three related wings of aspect ratio 2.83	Next

Bound With Arc R&M3262-68 Lack No.3269

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