NASA Technical Note [D271-280]
Contributor(s): Johnson, Donald F | Signorelli, Robert A | Waters, William J | Johnston, James R | Kramer, John L | Lowell, Herman H | Roudebush, William H | Black, Dugald O | King, Charles R. Biermann, Arnold E. Shinko, William G | Liebert, Curt H. Hatch, James E. Grant, Ronald W | McConnell, Dudley George | Englert, Gerald W | Mull, Harold R | Algranti, Joseph S.
Material type:
BookSeries: National Aeronautics and Space Administration (NASA) ; NASA Technical Note. Subject(s): Elastic-Plastic Stress | 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
| Item type | Current location | Collection | Call number | Status | Date due | Barcode | Item holds |
|---|---|---|---|---|---|---|---|
Technical Report
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PK Kelkar Library, IIT Kanpur | COMPACT STORAGE (BASEMENT) | Not for loan | 63651 |
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
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