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USE OF PILOT - TUBES IN THE MEASURMENT OF LAMINAR BOUNDARY LAYERS IN SUPERSONIC FLOW

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BookPublisher: Her Majesty'S Stationery Office,London 1957Description: 24.DDC classification: HMSO-R&M-3056 | -

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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	HMSO-R&M-3056 - (Browse shelf)	Not for loan		TR8899

Total holds: 0

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Previous	HMSO-R&M-3052 - ON THE STRESSING OF MULTI-RIP THIN WINGS OF LOW ASPECT RATIO AND RECTANGULAR PLAN-FORM	HMSO-R&M-3053 - SOME EXPERIMENTS WITH SONIC THROATS DOWNSTREAM FROM THE WORKING-SECTION OF A SLOTTED-WALL HIGH-SPEED TUNNEL	HMSO-R&M-3055 - A THEORETICAL AND EXPERIMENTAL INVESTIGATION OF THE FLOW OVER A FAMILY OF RECTANGULAR WINGS OF BICONVEX SECTION AT M=1.42	HMSO-R&M-3056 - USE OF PILOT - TUBES IN THE MEASURMENT OF LAMINAR BOUNDARY LAYERS IN SUPERSONIC FLOW	HMSO-R&M-3057 - ON THE INTEGRAL EQUATIONS OF TWO-DIMENSIONAL SUBSONIC FLUTTER DERIVATIVE THEORY	HMSO-R&M-3058 - ACCURACY OF MEASURMENT OF TURBULENT SKIN FRICTION BY MEANS OF SURFACE PITOT-TUBES AND THE DISTRIBUTION OF SKIN FRICTION ON A FLAT PLATE	HMSO-R&M-3059 - CALCULATION OF DERIVATIVES FOR A CROPPED DELTA WING WITH AN OSCILLATING CONSTANT-CHORD FLAP IN A SUPERSONIC AIR STREAM	Next

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