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USE OF CONICAL CAMBER TO PRODUCE FLOW ATTACHMENT AT THE LEADING EDGE OF A DELTA WING AND TO MINIMIZE LIFT-DEPENDENT DRAG AT SONIC AND SUPERSONIC SPEEDS

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BookPublisher: Her Majesty'S Stationery Office,London 1963Description: 32.DDC classification: ARC | R&M 3289

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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 3289 (Browse shelf)	Not for loan		TR16767

Total holds: 0

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Previous	ARC R&M 3286 An investigation of the flow about a plane half-wing of cropped-delta planform and 6 per cent symmetrical section at stream mach numbers between 0.8 and 1.41	ARC R&M 3287 Comparision of results in the A.R.E. transonic tunnel on a small and a large model of a slender wing	ARC R&M 3288 Experiments on a delta wing with jet-assisted lift	ARC R&M 3289 USE OF CONICAL CAMBER TO PRODUCE FLOW ATTACHMENT AT THE LEADING EDGE OF A DELTA WING AND TO MINIMIZE LIFT-DEPENDENT DRAG AT SONIC AND SUPERSONIC SPEEDS	ARC R&M 3290 FREE-FLIGHT MEASUREMENTS OF PRESSURE DISTRIBUTION AT TRANSONIC AND SUPERSONIC SPEEDS ON BODIES OF REVOLUTION HAVING PARABOLIC AFTERBODIES	ARC R&M 3292 FURTHER RESULTS ON THE MIXING OF FREE AXIALLY-SYMMETRICAL JETS OF MACH NUMBER 1.40	ARC R&M 3293 CHARTS OF PEAK AMPLITUDES IN INCIDENCE AND SIDESLIP IN ROLLING MANOEUVRES DUE TO INERTIA CROSS COUPLING	Next

Bound With Arc R&M3271-88,3290

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