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A THREE COMPONENT GUN TUNNEL BALANCE DESIGNED FOR TESTING THIN DELTA WINGS

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BookPublisher: Her Majesty'S Stationery Office, London 1971Description: 34.DDC classification: ARC | R&M 3664

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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 3664 (Browse shelf)	Not for loan Untraceable		TR17005

Total holds: 0

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Previous	ARC R&M 3661 MEASUREMENTS OF SECTION PRESSURE DISTRIBUTION AT A MACH NUMBER OF 2.0 ON A WING OF 70 DEGREES SWEEP MOUNTED ON A WAISTED BODY	ARC R&M 3662 A THEORETICAL STUDY OF HEIGHT CONTROL IN FLIGHT CLOSE TO THE GROUND AS AFFECTED BY ELEVATOR LIFT AND COCKPIT POSITION	ARC R&M 3663 BOUNDARY-LAYER SUCTION TO ELIMINATE CORNER SEPARATION IN CASCADES OF AEROFOILS	ARC R&M 3664 A THREE COMPONENT GUN TUNNEL BALANCE DESIGNED FOR TESTING THIN DELTA WINGS	ARC R&M 3665 AIRCRAFT CENTRE OF GRAVITY RESPONSE TO TWO-DIMENSIONAL SPECTRA OF TURBULENCE	ARC R&M 3666 SOME COMMENTS ON AIR CONDENSATION EFFECTS IN A HYPERSONIC HELIUM TUNNEL	ARC R&M 3667 THE VELOCITIES INDUCED BY DISTRIBUTIONS OF INFINITE KINKED SOURCE AND VORTEX LINES REPRESENTING WINGS WITH SWEEP AND DIHEDRAL IN INCOMPRESSIBLE FLOW	Next

Bound With Arc R&M 3660-3663, 3665-3668

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