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PANEL FLUTTER TESTS ON FULL-SCALE X-15 LOWER VERTICAL STABILIZER AT MACH NUMBER OF 3.0

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BookPublisher: Nasa, Washington, D.C. 1962Description: 61.DDC classification: NASA | TN D-1385 -

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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 TN D-1385 - (Browse shelf)	Not for loan		TR9553

Total holds: 0

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Previous	NASA TN D-1382 - SLIPSTREAM FLOW AROUND SEVERAL TILT-WING VTOL AIRCRAFT MODELS OPERATING NEAR THE GROUND	NASA TN D-1383 - RADIATION EXPOSURE IN SUPERSONIC TRANSPORTS	NASA TN D-1384 - WIND-TUNNEL INVESTIGATION AT A MACH NUMBER OF 2.01 OF THE SONIC-BOOM CHARACTERISTICS OF THREE WIND-BODY COMBINATIONS DIFFERING IN WING LONGITUDINAL LACATION	NASA TN D-1385 - PANEL FLUTTER TESTS ON FULL-SCALE X-15 LOWER VERTICAL STABILIZER AT MACH NUMBER OF 3.0	NASA TN D-1386 - EXPERIMENTAL INVESTIGATION OF THE EFFECTS OF COMPRESSIVE STRESS ON THE FLUTTER OF A CURVED PANEL AND A FLAT PANEL AT SUPERSONIC MACH NUMBERS	NASA TN D-1387 - ATMOSPHERE AS A PART OF THE SPACE ENVIRONMENT	NASA TN D-1388 - DRAG CHARACTERISTICS AND DYNAMIC STABILITY IN DESCENT OF A ROTARY PARACHUTE TESTED IN A VERTICAL TUNNEL	Next

Bound With Nasa Tn D-1381-90

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