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THE CALIBRATION OF A 60 DEGREE CONE TO MEASURE MACH NUMBER, TOTAL PRESSURE AND FLOW ANGLES AT SUPERSONIC SPEEDS.

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BookPublisher: Her Majesty'S Stationery Office, London 1963Description: 10.DDC classification: ARC | C.P. 628

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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. 628 (Browse shelf)	Not for loan		TR10615

Total holds: 0

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Previous	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.	ARC C.P. 630 SOME CHARACTERISTICS OF RECTANGULAR MULTI-SHOCK AND ISENTROPIC EXTERNAL COMPRESSION INTAKES AT A MACH NUMBER OF 2.9	ARC C.P. 673 MEASUREMENT OF LIFT AND PITCHING MOMENT ON FOUR OGEE WINGS AT SUPERSONIC SPEEDS	ARC C.P. 674 FORCES ON TETHERED RALLISTIC MISSILES DUE TO MOTOR CUT-OFF- A THEORETICAL TREATMENT	Next

Bound With Arc C.P.621-27, 629-30 Lack No.623-24

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