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THE AERODYNAMIC DERIVATIVES WITH RESPECT TO A RATE OF YAW FOR A DELTA WING WITH DIHEDRAL AND AT INCIDENCE AT SUPERSONIC SPEEDS

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BookPublisher: Her Majesty'S Stationery Office, London 1957Description: 23.DDC classification: ARC | R&M 2887

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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 R&M 2887 (Browse shelf)	Not for loan		TR18143

Total holds: 0

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Previous	ARC R&M 2883 AN EXPERIMENTAL INVESTIGATION OF A THICK-AEROFOIL NOZZLE CASCADE	ARC R&M 2885 MULTHOPP'S SUBSONIC LIFTING-SURFACE THEORY OF WINGS IN PITCHING OSCILLATIONS	ARC R&M 2886 PRESSURE AND BOUNDARY-LAYER MEASUREMENTS ON A TWO-DIMENSIONAL WING AT LOW SPEED	ARC R&M 2887 THE AERODYNAMIC DERIVATIVES WITH RESPECT TO A RATE OF YAW FOR A DELTA WING WITH DIHEDRAL AND AT INCIDENCE AT SUPERSONIC SPEEDS	ARC R&M 2888 CALCULATION OF THE PRESSURE DISTRIBUTION OVER A WING AT SONIC SPEEDS	ARC R&M 2889 THEORETICAL LOAD DISTRIBUTION ON A WING WITH A CYLINDRICAL BODY AT ONE END	ARC R&M 2895 ROLLING POWER MEASUREMENTS AND COMPARATIVE CALCULATIONS FOR FLEXIBLE MODEL WING CONSTRUCTED FROM XYLONITE	Next

Bound With Arc R&M2881-86,2888-99 Lack No.2884,2890-94,2896

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