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MEASUREMENTS IN A THREE-DIMENSIONAL TURBULENT BOUNDARY LAYER IN SUPERSONIC FLOW

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BookPublisher: Her Majesty'S Stationery Office, London 1966Description: 50.DDC classification: ARC | R&M 3537

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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 3537 (Browse shelf)	Not for loan Untraceable		TR14525

Total holds: 0

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Previous	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	ARC R&M 3539 THE DESIGN OF COMPRESSION SURFACES FOR HIGH SUPERSONIC SPEEDS USING CONICAL FLOW FIELDS	ARC R&M 3540 ALLEVIATION OF LEADING-EDGE HEATING BY CONDUCTION AND RADIATION	Next

Bound With Arc R&M 3531-3536,3538-3540,Lack No. 3533,35

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