| 000 | 00609 a2200241 4500 | ||
|---|---|---|---|
| 001 | 270938 | ||
| 020 | _a | ||
| 041 | _aeng | ||
| 080 | _aLNASA CR 3837 : 1984 | ||
| 245 | _aHeat transfer and pressure drop in blade cooling channels with turbulence promoters | ||
| 250 | _a | ||
| 260 | _aWashington, D.C. | ||
| 260 | _bNational Aeronautics and Space Administration (NASA) | ||
| 260 | _c1984 | ||
| 300 | _a153 p. | ||
| 300 | _c | ||
| 856 | _u | ||
| 490 | _aNASA CR 3837 : 1984 | ||
| 700 | _a | ||
| 650 | _a | ||
| 650 | _aTurbine blade, Heat transfer, Augmentation, Turbulent heat transfer | ||
| 942 | _cPP | ||
| 942 | _2UDC | ||
| 999 |
_c225569 _d225569 |
||