000 | 00707 a2200241 4500 | ||
---|---|---|---|
001 | 304350 | ||
020 | _a | ||
041 | _aeng | ||
080 | _aLNASA TN D 3289 : 1975 | ||
245 | _aCold-air investigation of a 3 1/2-stage fan-drive turbine with a stage loading factory of 4 designed for an integral lift engine : I - Turbine design and performance of first stage | ||
250 | _a | ||
260 | _aWashington, D.C. | ||
260 | _bNational Aeroronautic and Space Administration (NASA) | ||
260 | _c1975 | ||
300 | _a38 p. | ||
300 | _c | ||
856 | _uNASA | ||
490 | _aNASA TN D 3289 : 1975 | ||
700 | _a | ||
650 | _a | ||
650 | _aTurbine aerodynamics, High stage loading, Fan drive turbines | ||
942 | _cPP | ||
942 | _2UDC | ||
999 |
_c252858 _d252858 |