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Flow pattern on a tapered sweptback wing at mach numbers between 0.6 and 1.6

By: I M Hall.

Contributor(s): E W.E. Rogers.

Material type: materialTypeLabel

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BookPublisher: DDC classification: ARC | R&M 3271

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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 3271 (Browse shelf)	Not for loan		67683

Total holds: 0

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Previous	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 3271 Flow pattern on a tapered sweptback wing at mach numbers between 0.6 and 1.6	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

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