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WIND-TUNNEL TESTS ON THE EFFECTS OF AN ADDED MASS ON THE FLUTTER OF A MODEL DELTA WING. PART- 1. FIXED ROOT FLUTTER TESTS.PART-11.ANTI-SYMMETRIC FLUTTER TESTS.PART 111.SYMMETRIC FLUTTER TESTS.

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BookPublisher: Her Majesty'S Stationery Office, London 1958Description: 41.DDC classification: ARC-R&M | 3255

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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 3255 (Browse shelf)	Not for loan Untraceable		TR10495

Total holds: 0

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Previous	ARC-R&M 3252 TURBULENT WALL JETS WITH AND WITHOUT AN EXTERNAL STREAM.	ARC-R&M 3253 THE ANLYSIS OF BLADE VIBRATION DUE TO RANDOM EXCITATION.	ARC-R&M 3254 FORCE AND MOMENT COEFFICIENTS FOR VIBRATING AEROFOLIS IN CASCADE.	ARC-R&M 3255 WIND-TUNNEL TESTS ON THE EFFECTS OF AN ADDED MASS ON THE FLUTTER OF A MODEL DELTA WING. PART- 1. FIXED ROOT FLUTTER TESTS.PART-11.ANTI-SYMMETRIC FLUTTER TESTS.PART 111.SYMMETRIC FLUTTER TESTS.	ARC-R&M 3256 A NOTE ON FLUTTER OF ASYMMETRIC CONTROLS.	ARC-R&M 3257 MEASUREMENTS OF THE DIRECT PITCHING-MOMENT DERIVATIVES FOR TWO-DIMENSIONAL FLOW AT SUBSONIC AND SUPERSONIC SPEEDS AND FOR A WING OF ASPECT RATIO 4 AT SUBSONIC SPEEDS	ARC-R&M 3258 SOME POSSIBLE EFFECTS OF TRANSONIC SPEEDS ON WING-AILERON FLUTTER.	Next

Bound With: Arc R&M3241-3254,3256-3260.

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