000 00611nam a22001817a 4500
003 OSt
005 20210315111418.0
008 210315b xxu||||| |||| 00| 0 eng d
040 _cIIT Kanpur
041 _aeng
100 _aKremzier, Email J.
245 _aA method for evaluating the effects of drag and inlet pressure recovery on propulsion system performance [ Technical Note 3261 ]
_cEmail J. Kremzier
260 _aWashington
_bNational Advisory committee for Aeronautics
_c1954
300 _a21p
440 _aNational Advisory committee for Aeronautics (NACA)
650 _aPressure
942 _cREF
999 _c564320
_d564320