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A METHOD FOR CALCULATING THE PRESSURE DISTRIBUTION OF A BODY OF REVOLUTION MOVING IN A CIRCULAR PATH THROUGH A PERFECT INCOMPRESSIBLE FLUID.

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BookPublisher: Her Majesty'S Stationery Office, London 1960Description: 69.DDC classification: ARC | R&M 3139

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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 3139 (Browse shelf)	Not for loan		TR10765

Total holds: 0

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Previous	ARC R&M 3136 SECONDARY FLOW AND LOSSES IN A COMPRESSOR CASCADE	ARC R&M 3137 THE CALCULATION OF LIFE SLOPES,ALLOWING FOR BOUNDARY LAYER, WITH APPLICATIONS TO THE RAE 101AND 104 AEROFOILS.	ARC R&M 3138 SOME EXPLORATORY JET-FLAP TESTS ON A 60-DEG DELTA WING.	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.	Next

Bound With Arc R&M 3100-38, 3140 Lack No 3101-31

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