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A NUMERICAL METHOD FOR CALCULATING THE PRESSURE DUE TO THICKNESS ON SYMMETRICAL WINGS AT ZERO INCIDENCE IN SUPERSONIC FLOW

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BookPublisher: Her Majesty'S Stationery Office, London 1968Description: 49.DDC classification: ARC | R&M 3535

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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 3535 (Browse shelf)	Not for loan Untraceable		TR17086

Total holds: 0

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Previous	ARC R&M 3520 THE VARIATION OF PROFILE DRAG WITH MACH NUMBER UP TO THE CRITICAL VALUE; A COMPARISON OF RECENT PREDICTIONS WITH EARLY FLIGHT AND WIND-TUNNEL MEASUREMENTS AND A COMMENT ON AN EARLIER PREDICTION	ARC R&M 3532 ON TH FORMATION OF WHITE-LIGHT FRINGES IN A MACH-ZEHNDER INTERFEROMETER	ARC R&M 3534 GENERALISED AIRFORCES ON A CYLINDRICAL SHELL OSCILLATING HARMONICALLY IN A UNIFORM FLOW	ARC R&M 3535 A NUMERICAL METHOD FOR CALCULATING THE PRESSURE DUE TO THICKNESS ON SYMMETRICAL WINGS AT ZERO INCIDENCE IN SUPERSONIC FLOW	ARC R&M 3536 WHIRL OF AN AIRCRAFT POWER-PLANT INSTALLATION AND ITS INTERACTION WITH THE FLUTTER MOTION OF A FLEXIBLE WING	ARC R&M 3537 MEASUREMENTS IN A THREE-DIMENSIONAL TURBULENT BOUNDARY LAYER IN SUPERSONIC FLOW	ARC R&M 3538 MEASUREMENTS OF THE PERFORMANCE OF A TURBO-JET ENGINE WITH REHEAT (ROLLS ROYCE RA28R AVOL) IN HIGH-SPEED FLIGHT AND UNDER SIMULATED CONDITIONS IN TEST BEDS	Next

Bound With Arc R&M3533,3542-49 Lack No.3534,3536-41,3547

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