000 00593 a2200253 4500
001 138465
020 _a5
041 _aeng
080 _a621.438:621.17 Lie
245 _aFilm cooling with ejection from a row of inclined circular holes : an experimental study for the application to gas turbine blades
250 _a
260 _an.p.
260 _bn.p.,
260 _c1973
300 _avarious p.
300 _c29 cm
490 _aNASA TP 2201 : 1983
100 _aLiess, Christian
700 _a
650 _a
650 _aGas-turbines-Blades
942 _cBK
942 _2UDC
999 _c65043
_d65044