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A WIND-TUNNEL INVESTIGATION OF THE DIRECTIONAL AND LONGITUDINAL STABILITY OF THE JAVELIN AIRCRAFT AT TRANSONIC SPEEDS, INCLUDING COMPARISON WITH FLIGHT TEST RESULTS

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BookPublisher: Her Majesty'S Stationery Office, London 1965Description: 54.DDC classification: ARC | R&M 3403

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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 3403 (Browse shelf)	Not for loan		TR17079

Total holds: 0

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Previous	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.	ARC R&M 3399 NOTES AND COMMENTS ON SOME PARTICULAR FEATURES OF WIND-TUNNEL DESIGN FOLLOWING MEASUREMENTS OF FLOW DISTRIBUTION, WALL PRESSURES. IN THE N.P.L. 7FT (LOW TURBULENCE) WIND TUNNEL.	ARC R&M 3403 A WIND-TUNNEL INVESTIGATION OF THE DIRECTIONAL AND LONGITUDINAL STABILITY OF THE JAVELIN AIRCRAFT AT TRANSONIC SPEEDS, INCLUDING COMPARISON WITH FLIGHT TEST RESULTS	ARC R&M 3404 MECHANICAL ASPECTS OF TURBINE BLADE COOLING	ARC R&M 3405 AN EXPERIMENTAL HIGH-TEMPERATURE TURBINE (NO. 126)	ARC R&M 3409 CALCULATION OF UNSTEADY GENERALISED AIRFORCES ON A THIN WING OSCILLATING HARMONICALLY IN SUBSONIC FLOW	Next

Bound With 3401, 3404-3470, Lack No.3401-2,6-8,3411-59,61-69

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