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040 _cIIT Kanpur
041 _aeng
100 _aColladay, S. Raymond
245 _aThermal feasibility of using methane or hydrogen fuel for direct cooling of a first-stage turbing stator. [NASA TN D-6042]. [ NASA TN D-6042]
_cRaymond S. Colladay
260 _aWashington, D. C
_bNASA
_c1970
300 _a23p
440 _aNational Aeronautics and Space Administration (NASA)
505 _aNASA technical report
650 _aTurbines
650 _aMethane--Thermal properties
700 _aColladay, S. Raymond
942 _cTR
999 _c563378
_d563378