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COMPUTER PROGRAMMES TO CALCULATE THE RESPONSE OF FLEXIBLE AIRCRAFT TO GUSTS AND CONTROL MOVEMENTS.

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BookPublisher: Her Majesty'S Stationery Office, London 1966Description: 50.DDC classification: ARC | C.P. 957

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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. 957 (Browse shelf)	Not for loan		TR10849

Total holds: 0

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Previous	ARC C.P. 954 MEASUREMENTS OF WING BUFFETING ON A SCIMITAR MODEL.	ARC C.P. 955 MEASUREMENTS AT TRANSONIC SPEEDS OF THE SIDEFORCE & YAWING MOMENT ON VARIOUS STORE ARRANGEMENTS MOUNTED BENEATH A 45 DEGREE SWEPT WING-FUSELAGE MODEL.	ARC C.P. 956 NITROGEN CONSIDERATION IN THE R.A.R.D.E. HYPERSONIC GUN TUNNEL.	ARC C.P. 957 COMPUTER PROGRAMMES TO CALCULATE THE RESPONSE OF FLEXIBLE AIRCRAFT TO GUSTS AND CONTROL MOVEMENTS.	ARC C.P. 958 MEASUREMENTS OR DRAG, BASE PRESSURE AND BASE AERODYNAMIC HEAT TRANSFERN APPROPRIATE TO 8.5 DEGREE SEMI-ANGLE SHARP CONES IN FREE FLIGHT AT MACH NUMBERS FROM 0.8 TO 3.8.	ARC C.P. 959 THE INFLUENCE OF GAS STREAMS AND MAGNETIC FIELDS ON ELECTRIC DISCHARGES PART 3. ARCS IN TRANSVERSE MAGNETIC FIELDS AT ATMOSPHERIC PRESSURE.	ARC C.P. 960 FREE-FLIGHT MEASUREMENTS OF THE INCREMENTAL DRAG DUE TO ENGINE NACELLES ON A TRANSONIC SWEPT-WING AIRCRAFT.	Next

Bound With Arc C.P. 951-56, 958-60

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