| 000 | 00651 a2200241 4500 | ||
|---|---|---|---|
| 001 | 305979 | ||
| 020 | _a | ||
| 041 | _aeng | ||
| 080 | _aLNASA TP - 1603 : 1980 | ||
| 245 | _aComputer program for generating input for analysis of impingement cooled, axial-flow turbine blade | ||
| 250 | _a | ||
| 260 | _aWashington, D.C. | ||
| 260 | _bNational Aeronautics and Space Administration | ||
| 260 | _c1980 | ||
| 300 | _a55 p. | ||
| 300 | _c | ||
| 856 | _u | ||
| 490 | _aNASA TP - 1603 : 1980 | ||
| 700 | _a | ||
| 650 | _a | ||
| 650 | _aComputerized design, Aerodynamic configurations, Flow geometry, Profiles, Finite difference theory | ||
| 942 | _cPP | ||
| 942 | _2UDC | ||
| 999 |
_c254488 _d254488 |
||