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CALCULATION OF UNSTEADY GENERALISED AIRFORCES ON A THIN WING OSCILLATING HARMONICALLY IN SUBSONIC FLOW

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BookPublisher: Her Majesty'S Stationery Office, London 1965Description: 52.DDC classification: ARC | R&M 3409

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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 3409 (Browse shelf)	Not for loan		TR17082

Total holds: 0

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Previous	ARC R&M 3403 A WIND-TUNNEL INVESTIGATION OF THE DIRECTIONAL AND LONGITUDINAL STABILITY OF THE JAVELIN AIRCRAFT AT TRANSONIC SPEEDS, INCLUDING COMPARISON WITH FLIGHT TEST RESULTS	ARC R&M 3404 MECHANICAL ASPECTS OF TURBINE BLADE COOLING	ARC R&M 3405 AN EXPERIMENTAL HIGH-TEMPERATURE TURBINE (NO. 126)	ARC R&M 3409 CALCULATION OF UNSTEADY GENERALISED AIRFORCES ON A THIN WING OSCILLATING HARMONICALLY IN SUBSONIC FLOW	ARC R&M 3410 SOME EXPLORATORY MEASUREMENTS OF LEADING-EDGE VORTEX POSITIONS ON A DELTA WING OSCILLATING IN HEAVE	ARC R&M 3419 MEASUREMENTS OF THE DIRECT PITCHING-MOMENT DERIVATIVES FOR THREE WING PLANFORMS AT HIGH SUBSONIC SPEEDS	ARC R&M 3420 FLIGHT MEASUREMENTS OF THE DRAG OF A SWEPT-WING AIRCRAFT(HUNTER MK.I) AT MACH NUMBERS UP TO 1.2,TOGETHER WITH SOME MEASUREMENTS OF LIFT-CURVE SLOPE	Next

Bound With Arc R&M 3401-3405, 3410-3470, Lack No.3401-2,6-8,3411-59,61-69

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