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MEASUREMENTS THE DIRECT HINGS-MOMENT DERIVATIVES AT SUBSONIC AND TRANSONIC SPEEDS FOR A CROPPED DELTA WING WITH OSCILLATING FLAP.

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BookPublisher: Her Majesty'S Stationery Office,London 1957Description: 22.DDC classification: ARC | R&M 3163

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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 3163 (Browse shelf)	Not for loan Untraceable		TR16859

Total holds: 0

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Previous	ARC R&M 3139 A METHOD FOR CALCULATING THE PRESSURE DISTRIBUTION OF A BODY OF REVOLUTION MOVING IN A CIRCULAR PATH THROUGH A PERFECT INCOMPRESSIBLE FLUID.	ARC R&M 3140 A.R.A 9-FT * 8-FT TRANSONIC WIND TUNNEL	ARC R&M 3162 PRESSURE FLUCATIONS NEAR A COLD,SMALL-SCALE AIR JET(MEASUREMENT OF SPACE CORRELATIONS)	ARC R&M 3163 MEASUREMENTS THE DIRECT HINGS-MOMENT DERIVATIVES AT SUBSONIC AND TRANSONIC SPEEDS FOR A CROPPED DELTA WING WITH OSCILLATING FLAP.	ARC R&M 3164 ACCURATE SOLUTIONS OF THE LAMINAR-BOUNDARY-LAYER EQUATIONS, FOR FLOWS HAVING A STAGNATION POINT AND SEPARATION	ARC R&M 3165 BALANCE AND PRESSURE MEASUREMENTS AT HIGH SUBSONIC SPEEDS ON A MODEL OF A SWEPT-WING AIRCRAFT (HAWKER P.1052) AND COMPARISONS WITH FLIGHT DATA	ARC R&M 3166 A NOTES ON TEST FACTORS	Next

Bound With Arc R&M-3161-3162,3164-3170.

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