000 00703pam a2200205a 44500
003 OSt
005 20221226092815.0
008 221226b xxu||||| |||| 00| 0 eng d
040 _cIIT Kanpur
041 _aeng
100 _aMarek, Cecil J.
245 1 _aSIMULTANEOUS FILM AND CONVECTION COOLING OF A PLATE INSERTED IN THE EXHAUST STREAM OF A GAS TURBINE COMBUSTOR [NASA TN D-7156]
260 _bNational Aeronautics and Space Administration
_c1973
_aWashington, D.C.
300 _a34p
440 _aNational Aeronautics and Space Administration
440 _aNASA Technical Note
500 _aBound vol. contains NASA TN D 7150-7159 Lack No. 53
650 _aTurbine combustors
942 _cTR
999 _c396655
_d396655