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VERTICAL ACCELERATION DUE TO STRUCTURAL VIBRATIONS OF A SLENDER AIRCRAFT FLYING IN CONTINUOUS TURBULENCE.

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BookPublisher: Her Majesty'S Stationery Office, London 1963DDC classification: ARC | C.P. 842

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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. 842 (Browse shelf)	Not for loan Untraceable		TR10529

Total holds: 0

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Previous	ARC C.P. 838 INTERIM REPORT ON LOW-SPEED FLIGHT TESTS OF A SLENDER-WING RESEARCH AIRCRAFT ( HANDLEY PAGE H.P. 115 )	ARC C.P. 839 THE INTERPRETATION OF STRAIN MEASUREMENTS FOR FLIGHT LOAD DETERMINATION	ARC C.P. 840 COMPARISON OF SEVEN WING BUFFET BOUNDARIES MEASURED IN WIND TUNNELS AND IN FLIGHT	ARC C.P. 842 VERTICAL ACCELERATION DUE TO STRUCTURAL VIBRATIONS OF A SLENDER AIRCRAFT FLYING IN CONTINUOUS TURBULENCE.	ARC C.P. 843 THE MAGNETIC DEFLECTION OF SHORT ARCS ROTATING BETWEEN ANNULAR ELECTRODES ABOVE AND BELOW ATMOSPHERIC PRESSURE.	ARC C.P. 845 THE LATERAL OSCILLATION OF SLENDER AIRCRAFT.	ARC C.P. 846 LOW-SPEED WIND-TUNNEL MEASUREMENTS OF THE LIFT, DRAG AND PITCHING MOMENT ON THREE SYMMERICAL SLENDER WING-BODY MODEL.	Next

Bound With Arc C.P.841, 843-50

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