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DYNAMIC STABILITY DERIVATIVES OF A SLENDER WING, A COMPARISON OF THEORY WITH FREE-FLIGHT MODEL TESTS AT NEAR-ZERO LIFT M = 0.8 TO 2.4

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BookPublisher: Her Majesty'S Stationery Office, London 1968Description: 67.DDC classification: HMSO-R&M-995 | -

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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-995 - (Browse shelf)	Not for loan Untraceable		TR9652

Total holds: 0

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Previous	HMSO-R&M-992 - MARCHING PROCEDURE FOR THE DETERMINATION OF INVISCID TWO-DIMENSIONAL SONIC FLOW PAST A BLUNT SYMMETRICAL BODY	HMSO-R&M-993 - CALCULATION OF SUB-CRITICAL PRESSURE DISTRIBUTION ON SYMMETRIC AEROFOILS AT ZERO INCIDENCE	HMSO-R&M-994 - Low-speed wind-tunnel investigation of the roll stability of a 1/5 scale model of the short SC 1 at large sideslip	HMSO-R&M-995 - DYNAMIC STABILITY DERIVATIVES OF A SLENDER WING, A COMPARISON OF THEORY WITH FREE-FLIGHT MODEL TESTS AT NEAR-ZERO LIFT M = 0.8 TO 2.4	HMSO-R&M-996 - CORRELATION OF VOLTAGE-CURRENT CHARACTERISTICS OF WALL-STABILISED, FREE-BURNING AND CROSS-FLOW ARCS	HMSO-R&M-998 - GRADIENT PROPERTIES OF A MODEL OF STATIONARY RANDOM TURBULENCE	HMSO-R&M-999 - INVESTIGATION OF THE ROLLING MOMENTS DUE TO SIDESLIP ON HIGH TAILPLANES AT SUBSONIC, TRANSONIC AND SUPERSONIC SPEEDS	Next

Bound With Hmso-R&M-991-99

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