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FURTHER MEASUREMENTS OF TRANSIENT PRESSURES ON A NARROW-DELTA WING DUE TO A VERTICAL GUST

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BookPublisher: Hmso, London 1968Description: 14.DDC classification: ARC | C. P. 1012

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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. 1012 (Browse shelf)	Not for loan Untraceable		TR14130

Total holds: 0

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Previous	ARC- R&M 3244 PRESSURE DISTRIBUTION AND SURFACE FLOW ON 5% AND 9% THICK WINGS WITH CURVED TIP AND 60 DEG SWEEPBACK	ARC 3204 THE EFFCT OF INTERNAL CONTRACTION, INITIAL RATE OF SUBSONIC DIFFUSION, AND COWL AND CENTREBODY SHAPE ON THE PRESSURE RECOVERY OF A CONICAL-CENTERBODY INTAKE AT SUPERSONIC SPEEDS.	ARC-A&M 3250 PUBLISHED REPORTS AND MEMORANDA OF THE AERONAUTICAL RESEARCH COUNCIL	ARC C. P. 1012 FURTHER MEASUREMENTS OF TRANSIENT PRESSURES ON A NARROW-DELTA WING DUE TO A VERTICAL GUST	ARC C. P. 622 QUALITATIVE SOLUTION OF THE STABILITY EQATION FOR A BOUNDARY LAYER IN CONTACT WITH VARIOUS FORMS OF FLEXIBLE SURFACE.	ARC C.P. 1001 THE PILOT`S SAFETY PROBLEM IN CATEGORY II OPERATIONS AND THE POTENTIAL CONTRIBUTION OF HEAD-UP DISPLAY.	ARC C.P. 1002 THE DEVELOPMENT AT CRANFIELD OF A FREE PISTON COMPRESSION SHOCK TUBE.	Next

Bound With Arc C.P.1010,1013-1020, Lack No. 1011

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