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THE CALCULATION OF TURBULENT BOUNDARY LAYERS WITH INJECTION

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BookPublisher: Her Majesty'S Stationery Office, London 1968Description: 46.DDC classification: ARC | R&M 3542

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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 3542 (Browse shelf)	Not for loan Untraceable		TR17087

Total holds: 0

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Previous	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	ARC R&M 3542 THE CALCULATION OF TURBULENT BOUNDARY LAYERS WITH INJECTION	ARC R&M 3543 MINIMUM DRAG SURFACES OF GIVEN LIFT WHICH SUPPORT TWO-DIMENSIONAL SUPERSONIC FLOW FIELDS	ARC R&M 3544 THE STABILITY OF ROTOR BLADE FLAPPING MOTION AT HIGH TIP SPEED RATIONS	ARC R&M 3545 A NUMERICAL SOLUTION OF THE ANALYSIS AND DESIGN PROBLEMS FOR THE FLOW PAST ONE OR MORE AEROFOILS OR CASCADES	Next

Bound With Arc R&M3533-35,3543-49 Lack No.3534,3536-41,3547

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