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BOUNDARY-LAYER DRAG OF BI-CONVEX WING SECTION WITH HEAT TRANSFER AT SUPERSONIC SPEEDS.

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BookPublisher: Her Majesty'S Stationery Office, London 1965Description: 43.DDC classification: ARC | R&M 3393

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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 3393 (Browse shelf)	Not for loan		TR10744

Total holds: 0

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Previous	ARC R&M 3388 THE EFFECT OF FORWARD SPEED ON THE INLET FLOW DISTRIBUTION AND PERFORMANCE OF LIFTING FAN INSTALLED IN A WING.	ARC R&M 3389 THE NOISE OF EJECTORS.	ARC R&M 3392 ON THE AXIAL COMPRESSION OF LONG, SLIGHTLY CURVED PANELS.	ARC R&M 3393 BOUNDARY-LAYER DRAG OF BI-CONVEX WING SECTION WITH HEAT TRANSFER AT SUPERSONIC SPEEDS.	ARC R&M 3395 UPWASH INTERFERENCE ON WINGS OF FINITE SPAN IN A RECTANGULAR WIND TUNNEL WITH CLOSED SIDE WALLS AND POROUS-SLOTTED FLOOR AND ROOF.	ARC R&M 3397 MEASUREMENTS OF DIRECT PITCHING OSCILLATION DERIVATIVES FOR THREE CROPPED DELTA AND THREE ARROWHEAD PLANFORMS AT SUBSONIC AND TRANSONIC SPEEDS.	ARC R&M 3398 THE CHANGE IN SHOCK-TUNNEL TAILORING MACH NUMBER DUE TO DRIVER GAS MIXTURES OF HELIUM AND NITROGEN.	Next

Bound With Arc R&M3381-92, 3395-99 Lack No.3387, 3390-91, 3394 And 3396

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