000 00574 a2200241 4500
001 316874
020 _a
041 _aeng
080 _aLNASA TP 1615 : 1979
245 _aExtension of similarity test procedures to cooled engine components with insulating ceramic coatings
250 _a
260 _aWashington,D.C.
260 _bNASA
260 _c1980
300 _a15 p.
300 _c
856 _u
490 _aNASA TP 1615 : 1979
700 _a
650 _a
650 _aSimilarity,Heat transfer,Gas turbine engines,Turbine temperatures
942 _cPP
942 _2UDC
999 _c263778
_d263778