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EFFECTS OF HEAT TRANSFER ON LAMINAR BOUNDARY-LAYER DEVELOPMENT UNDER PRESSURE GRADIENTS IN COMPRESSIBLE FLOW.

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BookPublisher: Her Majesty'S Stationery Office, London 1960Description: 35.DDC classification: ARC | R&M 3218

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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 3218 (Browse shelf)	Not for loan Untraceable		TR16015

Total holds: 0

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Previous	ARC R&M 3215 THE EFFECTS OF HUMIDITY ON LAMINAR RECOVERY TEMPERAATURE MEASUREMENTS IN SUPERSONIC FLOW OF AIR IN WIND TUNNELS.	ARC R&M 3216 THE RELEATIONSHIP BETWEEN THE DISCRETE GUST POWER SPECTRA PRESENTATIONS OF ATMOSPHERIC TURBULENCE, WITH A SUGGESTED MODEL OF LOW- ALTITUDE TURBULENCE	ARC R&M 3217 FORMULAE FOR CALCULATING THE CAMBER SURFACE OF THIN SWEPT-BACK WINGS OF ARBITRARY PLAN-FORM WITH SUBSONIC LEADING EDGES, AND SPECIFIED LOAD DISTRIBUTION	ARC R&M 3218 EFFECTS OF HEAT TRANSFER ON LAMINAR BOUNDARY-LAYER DEVELOPMENT UNDER PRESSURE GRADIENTS IN COMPRESSIBLE FLOW.	ARC R&M 3219 THE INTERFERENCE ON A THREE-DIMENSIONAL JET-FLAP WING IN A CLOSED WIND TUNNEL	ARC R&M 3243 FLIGHT TESTS TO INVESTIGATE THE DYNAMIC LATERAL-STABILITY CHARACTERISTICS OF A 45-DEG DELTA. CROPPED TO GIVE THREE ASPECT RATIOS	ARC-R&M 3245 THERMAL BUCKLING OF CIRCULAR PLATES.	Next

Bound With Arc R&M-3211-3217,3219-3220.

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