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INVESTIGATION OF THE LOW SUBSONIC FLIGHT CHARACTERISTICS OF A MODEL OF A FLAT-TOP HYPERSONIC-BOOST GLIDE CONFIGURATION HAVING AN ARROWHEAD WING

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BookPublisher: Nasa, Washington, D.C. 1959Description: 21.DDC classification: NASA | TM X-193

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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-193 (Browse shelf)	Not for loan Untraceable		TR13582

Total holds: 0

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Previous	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	NASA TM X-193 INVESTIGATION OF THE LOW SUBSONIC FLIGHT CHARACTERISTICS OF A MODEL OF A FLAT-TOP HYPERSONIC-BOOST GLIDE CONFIGURATION HAVING AN ARROWHEAD WING	NASA TM X-195 LAUNCH, LOW-SPEED, AND LANDING CHARACTERISTICS DETERMINED FROM THE FIRST FLIGHT OF THE NORTH AMERICAN X-15 RESEARCH AIRPLANE	NASA TM X-197 EXPERIMENTAL INVESTIGATION OF A TRANSONIC COMPRESSOR CASCADE AND TEST RESULTS FOR FOUR BLADE SECTIONS	NASA TM X-208 - HEAT TRANSFER TO 36.75(DEGREE) AND 45(DEGREE) SWEPT BLUNT LEADING EDGES IN FREE FLIGHT AT MACH NUMBERS FROM 1.70 TO 2.99 AND FROM 2.50 TO 4.05	Next

Bound With Nasa Tm X-182-91,195-97 Lack No.184-85,187-90,192,194,196

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