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OSCILLATORY PRESSURE MEASUREMENTS ON A FLEXIBLE SLENDER-WING MODEL AT LOW SUBSONIC SPEEDS

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BookPublisher: Her Majesty'S Stationery Office, London 1969Description: 33.DDC classification: ARC | R&M 3596

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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 3596 (Browse shelf)	Not for loan Untraceable		TR17075

Total holds: 0

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Previous	ARC R&M 3593 TESTS AT SUBSONIC AND SUPERSONIC SPEEDS ON A SLENDER CAMBERED WING WITH FIN, UNDERWING ENGINE NACELLES AND TRAILING -EDGE CONTROLS	ARC R&M 3594 A PILOTED SIMULATION OF THE TAKE-OFF OF A SUPERSONIC TRANSPORT AIRCRAFT, WITH AND WITHOUT A TAKE-OFF DIRECTOR	ARC R&M 3595 THE STRUCTURE AND BEHAVIOUR OF LAMINAR SEPARATION BUBBLES	ARC R&M 3596 OSCILLATORY PRESSURE MEASUREMENTS ON A FLEXIBLE SLENDER-WING MODEL AT LOW SUBSONIC SPEEDS	ARC R&M 3597 COMPARISON OF THREE METHODS FOR THE EVALUATION OF SUBSONIC LIFTING-SURFACE THEORY	ARC R&M 3598 HALF-SPEED BEARING WHIRL EXCITED BY A SINGLE PROPAGATING STALL CELL IN A MULTI-STAGE AXIAL-FLOW COMPRESSOR	ARC R&M 3599 THE EFFECTS OF CURVATURE ON THE TURBULENT BOUNDARY LAYER	Next

Bound With Arc R&M 3590-3595, 3597-3599

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