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USE OF EXPERIMENTAL STEADY-FLOW AERODYNAMIC PARAMETERS IN THE CALCULATION OF FLUTTER CHARACTERISTICS FOR FINITE-SPAN SWEPT OR UNSWEPT WINGS AT SUBSONIC, TRANSONIC, AND SUPERSONIC SPEEDS

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BookPublisher: Nasa, Washington, D.C. 1960Description: 51.DDC classification: NASA | TM X-183

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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	NASA TM X-183 (Browse shelf)	Not for loan Untraceable		TR13579

Total holds: 0

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Previous	NASA TM X-172 - AERODYNAMIC CHARACTERISTICS AT MACH NUMBERS OF 1.41 AND 2.01 OF A SERIES OF CRANKED WINGS RANGING IN ASPECT RATIO FROM 4.00 TO 1.74 IN COMBINATION WITH A BODY	NASA TM X-178 - EXPLORATORY INVESTIGATION AT MACH NUMBER OF 2.01 OF THE LONGITUDINAL STABILITY AND CONTROL CHARACTERISTICS OF A WINGED REENTRY CONFIGURATION	NASA TM X-179 - WIND-TUNNEL INVESTIGATION AT HIGH SUBSONIC SPEED OF THE STATIC LONGITUDINAL STABILITY CHARACTERISTICS OF A WINGED REENTRY VEHICLE HAVING A LARGE NEGATIVELY DEFLECTED FLAP-TYPE CONTROL SURFACE	NASA TM X-183 USE OF EXPERIMENTAL STEADY-FLOW AERODYNAMIC PARAMETERS IN THE CALCULATION OF FLUTTER CHARACTERISTICS FOR FINITE-SPAN SWEPT OR UNSWEPT WINGS AT SUBSONIC, TRANSONIC, AND SUPERSONIC SPEEDS	NASA TM X-186 TESTS OF AERODYNAMICALLY HEATED MULTIWEB WING STRUCTURES IN A FREE JET AT MACH NUMBER 2 FIVE ALUMINUM-ALLOY MODELS OF 20-INCH CHORD WITH 0.064-INCH-THICK SKIN, 0.025-INCH-THICK WEBS...ANGLE OF ATTACK	NASA TM X-19 HEAT-TRANSFER AND DRESSURE MEASUREMENTS ON A FLAT-FACE CYLINDER AT A MACH NUMBER RANGE OF 2.49 TO 4.44	NASA TM X-191 HYDRODYNAMIC AND AERODYNAMIC CHARACTERISTICS OF A MODEL OF A SUPERSONIC MULTIJET WATER-BASED AIRCRAFT EQUIPPED WITH SUPERCAVITATING HYDROFOILS	Next

Bound With Nasa Tm X-182,186-97 Lack No.184-85,187-90,192,194,196

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