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LOW-SPEED WIND-TUNNEL TESTS ON THE LIFT-DEPENDENT DRAG OF DELTA WINGS WITH CONICAL CAMBER

By: Kirkpatrick,D.L.T.

Contributor(s): Butterworth,P. J.

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BookSeries: Aeronautical Research Council Current Papers Cp No.1293. Publisher: Her Majestys Stationery Office, London 1974Description: 26.DDC classification: TR | CP-1293

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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	TR CP-1293 (Browse shelf)	Not for loan		TR3320

Total holds: 0

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Previous	TR CP-1289 STUDY OF SOLID STATE REMOTE CONTROL TECHNIQUES AS APPLIED TO THE REDESIGN OF THE ELECTRICAL SYSTEM IN A LARGE CIVIL AIRCRAFT	TR CP-1290 SHOCK CAPTURING METHOD FOR CALCULATING SUPERSONIC FLOW FIELDS	TR CP-1291 MEASUREMENT OF THE ITERNAL PERFORMANCE OF A RECTANGULAR AIR INTAKE MOUNTED ON A FUSELAGE AT MACH NUMBERS FROM 1.6 TO 2	TR CP-1293 LOW-SPEED WIND-TUNNEL TESTS ON THE LIFT-DEPENDENT DRAG OF DELTA WINGS WITH CONICAL CAMBER	TR CP-1297 VARIABILITY OF FATIGUE DAMAGE FROM FLIGHT TO FLIGHT	TR CP-1298 FLIGHT DETERMINATION OF THE RUDDER POWER AND DIRECTIONAL STABILITY OF THE FAIREY DELTA 2 AIRCRAFT USING A WINGTIP PARACHUTE	TR CP-1299 FLIGHT SIMULATION OF A WESSEX HELICOPTER A VALIDATION EXERCISE	Next

Bound With: Arc Cp No.1291-1300

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