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TEMPERATURE AND PRESSURE STUDIES IN THE RESERVIOR OF A REFLECTED-SHOCK HYPERSONIC TUNNEL.

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BookPublisher: Her Majesty'S Stationery Office, London 1967Description: 44.DDC classification: ARC-R&M | 3479

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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 3479 (Browse shelf)	Not for loan Untraceable		TR10783

Total holds: 0

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Previous	ARC-R&M 3476 SOME FLIGHT MEASUREMENTS OF CROSSWIND LANDINGS ON A SMALL DELTA AIRCRAFT(AVRO 707A) .	ARC-R&M 3477 THE DESIGN-POINT PERFORMANCE OF MODEL INERNAL-EXPANSION PROPELLING NOZZLES WITH AREA RATIOS UP TO 4.	ARC R&M 3478 SOME EXACT CALCULATIONS OF THE LIFT AND DRAG PRODUCED BY A WEDGE IN SUPERSONIC FLOW, EITHER DIRECTLY OR BY INTERFERENCE.	ARC-R&M 3479 TEMPERATURE AND PRESSURE STUDIES IN THE RESERVIOR OF A REFLECTED-SHOCK HYPERSONIC TUNNEL.	ARC-R&M 3480 TRANSONIC FLOW IN THE THROAT REGION OF AN ANNULAR NOZZLE WITH AN ARBITRARY SMOOTH PROFIL.	ARC R&M 3482 FLIGHT DETERMINATION OF WING FLOW PATTERNS AND BUFFET BOUNDARIES FOR THE FAIREY DELTA 2 AIRCRAFT AT MACH NUMBERS BETWEEN 0.4 AND 1.3, AND COMPARISON WITH WIND TUNNEL RESULTS	ARC R&M 3483 LEAKAGE AND SECONDARY FLOWS IN COMPRESSOR CASCADES	Next

Bound With:Arc R&M-3471-3478,3480.

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