PKK Library Search for 'au:"Dixon,Sidney C"'

VIBRATION AND AERODYNAMIC BUCKLING EXPERIMENTS FOR BLUNT TRUNCATED CONICAL SHELLS WITH RING SUPPORTED EDGES

By Miserentino,Robert. Nasa, Washington, D.C. 1972 . 33 , Bound With Nasa Tn D-6860-79

Place Hold on VIBRATION AND AERODYNAMIC BUCKLING EXPERIMENTS FOR BLUNT TRUNCATED CONICAL SHELLS WITH RING SUPPORTED EDGES

SUPERSONIC ASYMMETRIC FLUTTER AND DIVERGENCE OF TRUNCATED CONICAL SHELLS WITH RING-SUPPORTED EDGES

By Dixon,Sidney C. Nasa, Washington, D.C. 1971 . 24 , Bound With Nasa Tn D-6220-29

Place Hold on SUPERSONIC ASYMMETRIC FLUTTER AND DIVERGENCE OF TRUNCATED CONICAL SHELLS WITH RING-SUPPORTED EDGES

NASA Technical Note [NASA TN D-1948]: Application of transtability concept to flutter of finite panels and experimental results

Washington NASA 1963 . 34p , Bound together NASA TN D-1941 to 1950 | Bound vol. Acc. No. 65584 contains Acc. No. TR10692 to TR10700

Place Hold on NASA Technical Note [NASA TN D-1948]: Application of transtability concept to flutter of finite panels and experimental results

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

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

VIBRATION AND FLUTTER TESTS OF A PRESSURIZED THIN-WALLED TRUNCATED CONICAL SHELL

By Miserentino,Robert. Nasa, Washington, D.C. 1971 . 24 , Bound With Nasa Tn D-6100-6105,6107-6109

Place Hold on VIBRATION AND FLUTTER TESTS OF A PRESSURIZED THIN-WALLED TRUNCATED CONICAL SHELL

FLUTTER,VIBRATION,AND BUCKLING OF TRUNCATED ORTHOTHROPIC CONICAL SHEELS WITH GENERAILZED ELASTIC EDGE RESTRAINT.

By Dixon,Sidney C. Nasa, Washington, D.C. 1970 . 77 , Bpound With Nasa Tn D-5751-5758.

Place Hold on FLUTTER,VIBRATION,AND BUCKLING OF TRUNCATED ORTHOTHROPIC CONICAL SHEELS WITH GENERAILZED ELASTIC EDGE RESTRAINT.

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

Place Hold on EXPERIMENTAL PRESSURES AND TURBULENT HEAT TRANSFER COEFFICIENTS ASSOCIATED EITH SINUSODIAL

Experimental investigation at mach number 3.0 of the effects of thermal stress and buckling on the flutter of four bay aluminium alloy panels with length width ratios of 10 [NASA TN D-921]

By Dixon, Sidney C.. Washington, D. C. National Aeronautics and Space Administration 1961 . 28p

Place Hold on Experimental investigation at mach number 3.0 of the effects of thermal stress and buckling on the flutter of four bay aluminium alloy panels with length width ratios of 10 [NASA TN D-921]

Experimental investigation at mach number 3.0 of the effects of thermal stress and buckling on the flutter of four bay aluminium alloy panels with length width ratios of 10 [NASA TN D-921]

By Dixon, Sidney C.. Washington, D. C. National Aeronautics and Space Administration 1961 . 28p

Theoretical and experimental vibration and buckling results for blunt truncated conical shells with ring-supported edges [NASA TN D-7003]

By Dixon, Sidney C.. Washington, D. C. National Aeronautics and Space Administration 1970 . 32p

Place Hold on Theoretical and experimental vibration and buckling results for blunt truncated conical shells with ring-supported edges [NASA TN D-7003]

Caparison of panel futter results from approximate aerodymaic theory with results from exact inviscid theory and experiment [NASA TN D-3649]

By Dixon Sidney C.. Washington, D. C. National Aeronautics and Space Administration . 26p

Place Hold on Caparison of panel futter results from approximate aerodymaic theory with results from exact inviscid theory and experiment [NASA TN D-3649]

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

Place Hold on NASA Technical Note [D-3491-3500]