| 000 | 00671 a2200241 4500 | ||
|---|---|---|---|
| 001 | 263620 | ||
| 020 | _a | ||
| 041 | _aeng | ||
| 080 | _aLNASA CR 4145 : 1988 | ||
| 245 | _aTwo - equation low - reynolds - number turbulence modeling of transitional boundary layer flows characteristics of gas turbine blades | ||
| 250 | _a | ||
| 260 | _aWashington, D.C. | ||
| 260 | _bNational Aeronautics and Space Adminstration (NASA) | ||
| 260 | _c1988 | ||
| 300 | _a271 p. | ||
| 300 | _c | ||
| 856 | _u | ||
| 490 | _aNASA CR 4145 : 1988 | ||
| 700 | _a | ||
| 650 | _a | ||
| 650 | _aBy-pass transition, Turbine blades, Heat transfer, Turbulence models, Prediction | ||
| 942 | _cPP | ||
| 942 | _2UDC | ||
| 999 |
_c216525 _d216525 |
||