EFFECTS OF DIFFERENTIAL PRESSURE, THARMAL STRESS, AND BUCKLING ON FLUTTER OF FLAT PANELS WITH LENGHT-WIDTH RATIO OF 2

By Dixon,Sidney C. Nasa, Washington, D.C. 1963 . 18 , Bound With Nasa Tn D-2041-46, 2048-50

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EXPERIMENTAL PRESSURES AND TURBULENT HEAT TRANSFER COEFFICIENTS ASSOCIATED EITH SINUSODIAL

By Shore,Charles P,Dixon,Sidney C. Nasa, Washington, D.C. 1963 . 28 , Bound With Nasa Tn D-1621-1625.1627-1630.Lack No-1628

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NASA Technical Note [D-3491-3500]

Washington National Aeronautics and Space Administration (NASA) 1971 , NASA Technical Note [D-3491]: Temperature control unit for sounding rocket applications/ by kerstin Fredga and Robert S. Lee | NASA Technical Note [D-3492]: Approximation of reentry angles of attack for a spinning body from rate-gyro and accelerometer data/ by Charles H. Whitlock | NASA Technical Note [D-3493]:Low-speed tests of 50 degree-swept parawings applied to a 0.17-scale model of a manned flight vehicle/ by Frank M. Bugg | NASA Technical Note [D-3494]: Error detection and correction approach to the time decoding problem/ by A.M. Demmerle, T. J. Karras, and P. J. McCeney | NASA Technical Note [D-3495]: Analysis of tailored-interface operation of shock tubes with helium-driven planetary gases/ by William J. Loubsky and John O. Reller | NASA Technical Note [D-3496]: Gemini spacecraft parachute landing system/ by John Vincze | NASA Technical Note [D-3497]: On the dynamics of capillaries and the existence of plasma flow in the pericapillary lymph space/ by John T. Howe and Yvonne S. Sheaffer | NASA Technical Note [D-3498]: Flutter at mach 3 of thermally stressed panels and comparison with theory for panels with edge rotational restraint/ by John L. Shideler, Sidney C. Dixon, and Charles P. Shore | NASA Technical Note [D-3499]: Dynamic-model study of planetary-entry configurations in the langley spin tunnel/ Peter J. Costigan | NASA Technical Note [D-3500]: Supersonic flutter of flat rectangular orthotropic panels elastically restrained against edge rotation/ by Larry L. Erickson

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EFFECTS OF DIFFERENTIAL PRESSURE, THARMAL STRESS, AND BUCKLING ON FLUTTER OF FLAT PANELS WITH LENGHT-WIDTH RATIO OF 2

EXPERIMENTAL PRESSURES AND TURBULENT HEAT TRANSFER COEFFICIENTS ASSOCIATED EITH SINUSODIAL

NASA Technical Note [D-3491-3500]