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EFFECTS OF ANGLE OF ATTACK AND THICKNESS RATIO ON THE FLUTTER OF RIGID UNSWEPT DIAMOND-AIRFOIL-SECTION WING AT A MACH NUMBER OF 10.0

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BookPublisher: Nasa, Washington, D.C. 1962Description: 23.DDC classification: NASA | TN D-1380

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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-1380 (Browse shelf)	Not for loan		TR12901

Total holds: 0

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Previous	NASA TN D-1377 DESCRIPTION AND PRELIMINARY CALIBRATION TESTS OF A SMALL ARC-HEATED HYPERSONIC WIND TUNNEL	NASA TN D-1378 AERODYNAMIC HEATING AND BOUNDARY-LAYER TRANSITION ON A 1/10-POWER NOSE SHAPE IN FREE FLIGHT AT MACH NUMBERS UP TO 16 MULTIPLE 10 TO THE POWER 6	NASA TN D-1379 STATIC LONGITUDINAL STABILITY AND PERFORMANCE OF SEVERAL BALLISTIC SPACECRAFT CONFIGURATIONS IN HELIUM AT MACH NUMBER OF 24.5	NASA TN D-1380 EFFECTS OF ANGLE OF ATTACK AND THICKNESS RATIO ON THE FLUTTER OF RIGID UNSWEPT DIAMOND-AIRFOIL-SECTION WING AT A MACH NUMBER OF 10.0	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	Next

Bound With Nasa Tn D-1376-79

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