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WIND TUNNEL MEASUREMENTS OF THE LOW SPEED STALLING CHRACTERISTICS OF A MODEL OF THE HAWKER SIDDELEY TRIDENT IC

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BookPublisher: Her Majesty'S Stationery Office, London 1969Description: 57.DDC classification: ARC | R&M 3608

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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 3608 (Browse shelf)	Not for loan		TR16969

Total holds: 0

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Previous	ARC R&M 3603 CONDITIONS FOR THE EXISTENCE OF AN INTERIAL SUBRANGE IN TURBULENT FLOW	ARC R&M 3604 THE MEASUREMENT OF THE EFFECTS OF SLUSH AND WATER ON AIRCRAFT DURING TAKE-OFF.PART 1-THE TECHNIQUE	ARC R&M 3605 A SIMULATOR INVESTIGATION OF ROLLING REQUIREMENTS FOR LANDING APPROACH	ARC R&M 3608 WIND TUNNEL MEASUREMENTS OF THE LOW SPEED STALLING CHRACTERISTICS OF A MODEL OF THE HAWKER SIDDELEY TRIDENT IC	ARC R&M 3609 THE EQUATIONS MOTION OF A VISCOUS COMPRESSIBLE GAS REFERRED TO AN ARBITRARILY MOVING CO-ORDINATE SYSTEM	ARC R&M 3610 A COMPRARATIVE STUDY OF EXTRAPOLATION METHODS FOR CREEP DATA AT SMALL STRAINS	ARC R&M 3611 FLIGHT MEASUREMENTS OF GROUND EFFECT ON THE LIFT AND PITCHING MOMENT OF A LARGE TRANSPORT AIRCRAFT (COMET 3B) AND COMPARISON WITH TUNNEL AND OTHER DATA.	Next

Bound With Arc R&M-3600-3607,3609-3612.Lack No-3602,3606,3607.

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