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SLANDER NOT-SO-THIN WING THEORY

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BookPublisher: Her Majesty'S Stationery Office, London 1963Description: 29.DDC classification: HMSO-R&M-659 | -

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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-659 - (Browse shelf)	Not for loan		TR9032

Total holds: 0

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Previous	HMSO-R&M-656 - 8FT. X 6FT. TRANSONIC WIND TUNNEL TESTS ON A 1/24 SCALE MODEL OF THE FAIREY DELTA 2 (ER.103)	HMSO-R&M-657 - PRESSURE MEASUREMENTS ON A CONE-CYLINDER-FLARE CONFIGURATION AT M=6.85 AND INCIDENCE UP TO 30/CIRC	HMSO-R&M-658 - PROVING TESTS OF A WINGTIP PARACHUTE INSTALLATION ON A VENOM AIRCRAFT, WITH SOME MEASUREMENTS OF DIRECTIONAL STABILITY AND RUBBER POWER	HMSO-R&M-659 - SLANDER NOT-SO-THIN WING THEORY	HMSO-R&M-660 - ROOM TEMPERATURE INSTABILITY AND FRACTION IN ROTATING DISCS AND CORRELATION WITH BI-AXIAL TENSILE TEST DATA	HMSO-R&M-891 - PERFORMENCE OF A CONICAL CONVERGENT-DIVERGENT NOZZLE WITH AREA RATIO 2.9 IN EXTERNAL FLOW	HMSO-R&M-892 - EXPERIMENTAL INVESTIGATION OF THE INFLUENCE OF BASE BLEED ON THE BASE DRAG OF VARIOUS PROPERLING NOZZLE CONFIGURATIONS	Next

Bound With Hmso-R&M-651-60

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