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AN EXPERIMENTAL INVESTIGATION AT SUPERSONIC SPEEDS OF THE CHARACTERISTICS OF TWO GOTHIE WINGS, ONE PLANE AND ONE CAMBERED.

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BookPublisher: Her Majesty'S Stationery Office, London 1959Description: 32.DDC classification: ARC | R&M 3211

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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 3211 (Browse shelf)	Not for loan Untraceable		TR16008

Total holds: 0

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Previous	ARC R&M 3208 SUBSONIC WIND-TUNNEL TESTS ON A CRESCENT-WINGED AIRCRAFT, INCLUDING TESTS OF LEADING-EDGE DROOP DESIGNS AND SEVERAL TAILPLANE HEIGHTS.	ARC R&M 3209 AN EXPERIMENTAL INVESTIGATION OF THE TRANSONIC FLOW OVER AN UNSWEPT WING OF ASPECT RATIO 3.5, TAPER RATIO 0.5, WITH A 4 PERCENT BICONVEX SECTION.	ARC R&M 3210 ELEVATOR FLUTTER INVOLVING TWO TABS	ARC R&M 3211 AN EXPERIMENTAL INVESTIGATION AT SUPERSONIC SPEEDS OF THE CHARACTERISTICS OF TWO GOTHIE WINGS, ONE PLANE AND ONE CAMBERED.	ARC R&M 3212 A SUPERSONIC TUNNEL DESIGN FOR TESTING ENGINE INTAKES.	ARC R&M 3213 ABSTRACTS OF PAPERS PUBLISHED EXTERNALLY.	ARC R&M 3214 THEORETICAL SUBSONIC DERVATIVES FOR AN OSCILLATING M-WING	Next

Bound With Arc R&M 3201-3210,3212-3220.

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