| 000 | 00610 a2200241 4500 | ||
|---|---|---|---|
| 001 | 308204 | ||
| 020 | _a | ||
| 041 | _aeng | ||
| 080 | _aLNASA TM X 2133 : 1970 | ||
| 245 | _aCold-air investigation of a turbine with transpiration-cooled stator : part - 2 | ||
| 250 | _a | ||
| 260 | _aWashington, D.C. | ||
| 260 | _bNational Aeronautics and Space Administration | ||
| 260 | _c1970 | ||
| 300 | _a33 p. | ||
| 300 | _c | ||
| 856 | _uNASA | ||
| 490 | _aNASA TM X 2133 : 1970 | ||
| 700 | _a | ||
| 650 | _a | ||
| 650 | _aTurbine aerodynamics, Static cascade, Vane surface pressure distribution | ||
| 942 | _cPP | ||
| 942 | _2UDC | ||
| 999 |
_c256489 _d256489 |
||