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STABILITY AND CONTROL FLIGHT TESTING-SOME OF THE TEST INSTRUMENTATION REQUIREMENTS

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BookPublisher: Hmso, London 1968Description: 10.DDC classification: ARC | C.P. 1015

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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. 1015 (Browse shelf)	Not for loan Untraceable		TR14133

Total holds: 0

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Previous	ARC C.P. 1009 ATMOSPHERIC TURBULENCE AND AIRCRAFT HEIGHT-KEEPING ACCURACY.	ARC C.P. 1013 THE INFLUENCE OF DENSITY GRADIENTS ON THE EFFECTIVENESS OF FILM COOLING	ARC C.P. 1014 AERODYNAMIC CHARACTERISTICS AT M=4.3 OF MONOPLANE, TRIFORM AND CRUCIFORM SLENDER DELTA WING BODIES WITH ALL-MOVING TAIL CONTROL SURFACES	ARC C.P. 1015 STABILITY AND CONTROL FLIGHT TESTING-SOME OF THE TEST INSTRUMENTATION REQUIREMENTS	ARC C.P. 1016 FORCES ON CONE CYLINDERS AT M=3.98	ARC C.P. 1017 SOME NOTES ON FUEL BOILING LOSSES AND FUEL-TANK PRESSURISATION IN A LONG-RANGE SUPERSONIC AIRCRAFT	ARC C.P. 1018 MEASUREMENTS OF THE EFFECTS OF THICKNESS ON VORTEX BREAKDOWN POSITION ON A SERIES OF SHARP-EDGED DELTA WINGS	Next

Bound With Arc C.P.1010-1014,1016-1020,Lack No. 1011

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