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FREE-FLIGHT MEASUREMENTS OF THE INCREMENTAL DRAG DUE TO ENGINE NACELLES ON A TRANSONIC SWEPT-WING AIRCRAFT.

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BookPublisher: Her Majesty'S Stationery Office, London 1967Description: 19.DDC classification: ARC | C.P. 960

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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. 960 (Browse shelf)	Not for loan		TR10852

Total holds: 0

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Previous	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.	ARC C.P. 982 ON THE EQUILIBRIUM PISTON TECHNIQUE IN GUN TUNNELS	ARC C.P. 983 LOW-SPEED WIND-TUNNEL TESTS ON A 1/6TH SCALE MODEL OF AN AIR-CUSHION-VEHICLE (BRITTEN-NORMAN CUSHIONCRAFT C.C.2.)	ARC C.P. 984 DRAG MEASUREMENTS ON A SERIES OF AFTERBODIES AT TRANSONIC SPEEDS SHOWING THE EFFECT OF STING INTERFERENCE	Next

Bound With Arc C.P. 951-59

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