000			03468nam a22005897a 4500
003			OSt
040			_cIIT Kanpur
041			_aeng
245			_aNASA Technical Note D-1881, 1882, 1883, 1884, 1885, 1887, 1888, 1889,1890,
260			_aWashington, D.C. _bNASA _c1963
300			_aPage Vari.
440			_a National Aeronautics and Space Administration (NASA) ; NASA Technical Note.
500			_aNASA TN D-1881: Stress-strain behavior of Tungsten-fiber-reinforced copper composites/ David L. McDanels, Robert W. Jech, and John W.Weeton
500			_aNASA TN D-1882: Experimental investigation of chemical reaction between propellant tank material and rocket fuels or oxidizers when impacted by small high-velocity projectiles/ by Robert P. Dengler
500			_aNASA TN D-1883: Analytical and Experimental study of Pool heating of liquid hydrogen over a range of accelerations/ by Robert W. Graham, Robert C. Hendricks, and Robert C. Ehlers
500			_aNASA TN D-1884: Large-scale wind-tunnel tests in ground effect of a 35 degree sweptback wing jet transport model equipped with blowing boundary-layer-control trailing-and leading-edge flaps/ by Kiyoshi Aoyagi and David H. Hickey
500			_aNASA TN D-1885: Study of the nonequilibrium flow field behind normal shock waves in carbon dioxide/ by John T. Howe, John R. Viegas, and Yvonne S. Sheaffer
500			_aNASA TN D-1887: Full-scale wind-tunnel tests of a medium-weight utility helicopter at forward speeds/ by John L. McCloud, James C. Biggers, and Ralph L. Maki
500			_aNASA TN D-1888: Preliminary study of handling-qualities requirements of supersonic transports in high-speed cruising flight using piloted simulators/ by Maurice D. White, Richard F. Vomaske, Walter E. McNeill, and George E. Cooper
500			_aNASA TN D-1889: Influence of heating rate and test stream oxygen content onthe insulation efficiency/ by Nick S. Vojvodich and Earnest l. Winkler
500			_aNASA TN D-1890: Measurement of the heat transfer to bodies of revolution in free flight by use of a catcher calorimeter/ by Gary T. Chapman and Charles T. Jackson
650			_aWind-Tunnel Tests -- Ground Effect
650			_aSimulation Rocket -- Propellant Tank Material
650			_aTensile Properties -- Metallic Composites
653			_aLiquid Hydrogen
653			_aEarth Gravity -- Multigravities -- Pressure
653			_aShock Waves -- Nonequilibrium Flow
653			_aFuselage Attitudes -- Helicopter
653			_aCruising Flight -- Supersonic Transport
653			_aCold Wall Heat -- Insulation Efficiency
653			_aHemisphere -- Experimental Heating Rate
653			_aBlunted Cone -- Heat Transfer -- Experimental Technique
700			_a McDanels, David L.
700			_a Jech, Robert W.
700			_aWeeton, John W.
700			_aDengler, Robert P.
700			_a Graham, Robert W.
700			_a Hendricks, Robert C.
700			_a Ehlers, Robert C.
700			_aAoyagi, Kiyoshi
700			_aHickey, David H.
700			_aHowe, John T.
700			_a Viegas, John R.
700			_a Sheaffer, Yvonne S.
700			_aMcCloud, John L.
700			_a Biggers, James C.
700			_aMaki, Ralph L. _aWhite, Maurice D. _aVomaske, Richard F. _aMcNeill, Walter E. _aCooper, George E. _aVojvodich, Nick S.
700			_aWinkler, Earnest l.
700			_a Chapman, Gary T.
700			_a Jackson, Charles T.
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999			_c565762 _d565762