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DESIGN AND OPERATION OF THE N.G.T.E. THERMAL SHOCK ANALOGUE.

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BookPublisher: Her Majesty'S Stationery Office, London 1959Description: 14.DDC classification: ARC | C.P. 557

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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 C.P. 557 (Browse shelf)	Not for loan		TR11023

Total holds: 0

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Previous	ARC C.P. 554 BOUNDARY LAYER MEASUREMENTS AT LOW SPEED ON TWO WINGS OF 45 DEGREE AND 55 DEGREE SWEEP.	ARC C.P. 555 AN EXPERIMENTAL STUDY OF THE GLANCING INTERACTION BETWEEN A SHOCK WAVE AND A TURBULENT BOUNDARY LAYER.	ARC C.P. 556 SOME CALCULATIONS BY THE CROCCO-LEES AND OTHER METHODS OF INTERACTIONS BETWEEN SHOCK WAVES AND LAMINAR BOUNDARY LAYERS, INCLUDING EFFECTS OF HEAT TRANSFER AND SUCTION.	ARC C.P. 557 DESIGN AND OPERATION OF THE N.G.T.E. THERMAL SHOCK ANALOGUE.	ARC C.P. 558 A NOTE ON THE USE OF STEADY EXPANSIONS IN SHOCK TUBES AND SHOCK TUNNELS.	ARC C.P. 559 A PRELIMINARY STUDY OF IONIC RECOMBINATION OF ARGON IN WIND TUNNEL NOZZLES.	ARC C.P. 560 PRESSURE AND BOUNDARY LAYER MEASUREMENTS ON A TAPERED SWEPT WING IN FLIGHT.	Next

Bound With Arc C.P. 551-56, 558-60

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