| 000 | 00628 a2200241 4500 | ||
|---|---|---|---|
| 001 | 311917 | ||
| 020 | _a | ||
| 041 | _aeng | ||
| 080 | _aLNASA TM X 3471 : 1977 | ||
| 245 | _aAir cooling of disk of a solid integrally cast turbine rotor for an automotive gas turbine | ||
| 250 | _a | ||
| 260 | _aWashington, D.C. | ||
| 260 | _bNational Aeronautics & Space Administration | ||
| 260 | _c1977 | ||
| 300 | _a18 p. | ||
| 300 | _c | ||
| 856 | _uNASA | ||
| 490 | _aNASA TM X 3471 : 1977 | ||
| 700 | _a | ||
| 650 | _a | ||
| 650 | _aAutomobile engine, Air cooling, Turbine blade, Gas turbine engines, Heat transfer | ||
| 942 | _cPP | ||
| 942 | _2UDC | ||
| 999 |
_c260573 _d260573 |
||