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NOTES ON SOME EXPERIMENTAL AND THEORETICAL RESULTS FOR THE BOUNDARY LAYER DEVELOPMENT AFT OF THE SHOCK IN A SHOCK-TUBE.

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BookPublisher: Her Majesty'S Stationery Office, London 1963Description: 32.DDC classification: ARC | C.P. 625

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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. 625 (Browse shelf)	Not for loan		TR10612

Total holds: 0

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Previous	ARC C.P. 580 AN AMPLITUDE PROBABILITY ANALYSER FOR USE IN TURBULENCE AND NOISE MEASUREMENTS	ARC C.P. 589 OBSERVATIONS OF STALL CELLS IN A SINGLE STAGE COMPRESSOR.	ARC C.P. 590 THE 7IN. X 7IN. HYPERSONIC WIND TUNNEL AT R.A.E. FARNBOROUGH.	ARC C.P. 625 NOTES ON SOME EXPERIMENTAL AND THEORETICAL RESULTS FOR THE BOUNDARY LAYER DEVELOPMENT AFT OF THE SHOCK IN A SHOCK-TUBE.	ARC C.P. 626 .TABULATED SOLUTIONS OF THE EQUILIBRIUM GAS PROPERTIES BEHIND THE INCIDENT AND REFLECTED NORMAL SHOCK-WAVE IN A SHOCK-TUBE I-NITROGEN II-OXYGENE	ARC C.P. 627 AN INVESTIGATION OF WING-AILERON FLUTTER USING GROUND LAUNCHED ROCKET MODELS.	ARC C.P. 628 THE CALIBRATION OF A 60 DEGREE CONE TO MEASURE MACH NUMBER, TOTAL PRESSURE AND FLOW ANGLES AT SUPERSONIC SPEEDS.	Next

Bound With Arc C.P.621-22, 626-30 Lack No.623-24

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