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SOME TESTS ON AVON-CANBERRA INSTALLATION TO MEASURE THRUST IN FLIGHT.

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BookPublisher: Her Majesty'S Stationery Office, London 1955Description: 23.DDC classification: ARC | C.P. 518

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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. 518 (Browse shelf)	Not for loan		TR10945

Total holds: 0

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Previous	ARC C.P. 515 STATIC TESTS ON A CONICAL CENTREBODY SUPERSONIC AIR INTAKE WITH AN AUXILIARY AIR INLET SLOT.	ARC C.P. 516 AN APPROXIMATE METHOD FOR CALCULATING THE LAMINAR BOUNDARY LAYER ON AN INFINITE SWEPT WING WITH ARBITRARY VELOCITY AND SUCTION DISTRIBUTIONS.	ARC C.P. 517 WIND TUNNEL EXPERIMENTS ON A MODEL OF A TANDEM ROTOR HELICOPTER.	ARC C.P. 518 SOME TESTS ON AVON-CANBERRA INSTALLATION TO MEASURE THRUST IN FLIGHT.	ARC C.P. 519 WIND TUNNEL MEASUREMENTS OF THE LIFE-DEPENDENT DRAG OF THIN CONICALLY CAMBERED SLENDER DELTA WINGS AT MACH NUMBERS 1.4 AND 1.8	ARC C.P. 520 COMPARISON OF THEORETICAL AND MEASURED SURFACE FRESSURES AT M=1.2 ON THREE BODIES HAVING DIFFERENT WAISTINGS.	ARC C.P. 532 AUTOMATIC CONTROL OF LABORATORY REPRESENTATION OF KINETIC HEATING.	Next

Bound With Arc C.P.511-17, 519-20

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