NASA Technical Note [D271-280] 
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.- ( National Aeronautics and Space Administration (NASA) NASA Technical Note.    
<br/>NASA 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 NASA 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 NASA Technical Note D273: Numerical computation of aerodynamic heating of liquid propellants/by  John L. Kramer, Herman H. Lowell and William H. Roudebush NASA Technical Note D274: Crash-fire protection system for A J57 turbojet engine using water as a cooling and inerting agent/ by Dugald O. Black NASA Technical Note D275: Compilation of thermodynamic properties, transport properties, and theoretical rocket performance of gaseous hydrogen/ by Charles R. King NASA Technical Note D276: Performance study of a piston-type pump for liquid hydrogen/ by Arnold E. Biermann and William G. Shinko NASA 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 NASA Technical Note D278: Free-flight observation of a separated turbulent flow including heat transfer up to mach 8.5 / by Dudley George McConnell NASA Technical Note D279: Operational method of determining initial contour of and pressure field about a supersonic jet/ Gerald W. Englert NASA Technical Note D280: Flight measurement of wall-pressure fluctuations and boundary-layer turbulence/ by Harold R. Mull and Joseph S. Algranti 
<br/><u>Subject Headings:</u> <br/>Elastic-Plastic Stress;
<br/><label>Subjects--Index Terms: </label>Turbojet Engine Rocket Propellant Tanks Combustor Flame Crash-fire Protection System -- Turbojet Engine Rocket Propellant Liquid Nitrogen, Hydrogen Heat-Transfer Coefficients -- Rocket Engine Hemisphere-Cone-Cylinder Supersonic Jet -- Initial Contour Fighter Jet Aircraft -- Flight Test 
<br/><U>Author Added Entry: </u><br/>Johnson, Donald F. ;<br/> Signorelli, Robert A.;<br/>Waters, William J. ;<br/>Johnston, James R. ;<br/> Kramer, John L.;<br/> Lowell, Herman H.;<br/> Roudebush, William H.;<br/> Black, Dugald O.;<br/>King, Charles R. ;<br/>Biermann, Arnold E. ;<br/>Shinko, William G. ;<br/> Liebert, Curt H.;<br/> Hatch, James E.;<br/>Grant, Ronald W. ;<br/>McConnell, Dudley George ;<br/>Englert, Gerald W. ;<br/> Mull, Harold R. ;<br/>Algranti, Joseph S. ;
<br><U>Copy Details:</u><br> Acc. No.: <b>63651</b>, Full Call No.: ,   Item type:  Technical Report , Location: COMPACT STORAGE (BASEMENT), <br><b>------------------------- --------------------- ------ --------- ------- ------- --------- -------- </b><br>