| 000 | 03201nam a22005417a 4500 | ||
|---|---|---|---|
| 003 | OSt | ||
| 040 | _cIIT Kanpur | ||
| 041 | _aeng | ||
| 245 | _aNASA Technical Note [D271-280] | ||
| 440 | _aNational Aeronautics and Space Administration (NASA) | ||
| 440 | _a NASA Technical Note. | ||
| 500 | _aNASA Technical Note D271: Analysis of Elastic-plastic stress distribution in thin-wall cylinders and spheres subjected to internal pressure and nuclear radiation heating/ by Donald F. Johnson | ||
| 500 | _aNASA Technical Note D272: Thermal-stress fatigue cracking of turbine buckets operated at 1700 degree F in a turbojet engine with long periods of operation between starts/ by Robert A. Signorelli, James R. Johnston and William J. Waters | ||
| 500 | _aNASA Technical Note D273: Numerical computation of aerodynamic heating of liquid propellants/by John L. Kramer, Herman H. Lowell and William H. Roudebush | ||
| 500 | _aNASA Technical Note D274: Crash-fire protection system for A J57 turbojet engine using water as a cooling and inerting agent/ by Dugald O. Black | ||
| 500 | _aNASA Technical Note D275: Compilation of thermodynamic properties, transport properties, and theoretical rocket performance of gaseous hydrogen/ by Charles R. King | ||
| 500 | _aNASA Technical Note D276: Performance study of a piston-type pump for liquid hydrogen/ by Arnold E. Biermann and William G. Shinko | ||
| 500 | _aNASA Technical Note D277: Application of various techniques for determining local heat-trasfer coefficients in a rocket engine from transient experimental data / by Curt H. Liebert, James E. Hatch, and Ronald W. Grant | ||
| 500 | _aNASA Technical Note D278: Free-flight observation of a separated turbulent flow including heat transfer up to mach 8.5 / by Dudley George McConnell | ||
| 500 | _aNASA Technical Note D279: Operational method of determining initial contour of and pressure field about a supersonic jet/ Gerald W. Englert | ||
| 500 | _aNASA Technical Note D280: Flight measurement of wall-pressure fluctuations and boundary-layer turbulence/ by Harold R. Mull and Joseph S. Algranti | ||
| 650 | _aElastic-Plastic Stress | ||
| 653 | _aTurbojet Engine | ||
| 653 | _aRocket Propellant Tanks | ||
| 653 | _aCombustor Flame | ||
| 653 | _aCrash-fire Protection System -- Turbojet Engine | ||
| 653 | _aRocket Propellant | ||
| 653 | _aLiquid Nitrogen, Hydrogen | ||
| 653 | _aHeat-Transfer Coefficients -- Rocket Engine | ||
| 653 | _aHemisphere-Cone-Cylinder | ||
| 653 | _aSupersonic Jet -- Initial Contour | ||
| 653 | _aFighter Jet Aircraft -- Flight Test | ||
| 700 | _aJohnson, Donald F. | ||
| 700 | _a Signorelli, Robert A. | ||
| 700 | _aWaters, William J. | ||
| 700 | _aJohnston, James R. | ||
| 700 | _a Kramer, John L. | ||
| 700 | _a Lowell, Herman H. | ||
| 700 | _a Roudebush, William H. | ||
| 700 | _a Black, Dugald O. | ||
| 700 |
_aKing, Charles R. _aBiermann, Arnold E. _aShinko, William G. |
||
| 700 |
_a Liebert, Curt H. _a Hatch, James E. _aGrant, Ronald W. |
||
| 700 | _aMcConnell, Dudley George | ||
| 700 | _aEnglert, Gerald W. | ||
| 700 | _a Mull, Harold R. | ||
| 700 | _aAlgranti, Joseph S. | ||
| 942 | _cBK | ||
| 999 |
_c565961 _d565961 |
||