000 00518nam a22001697a 4500
005 20190626155451.0
008 190626b xxu||||| |||| 00| 0 eng d
040 _cIIT Kanpur
041 _aeng
082 _a629.505
_bD74r
100 _aFox,N.L.
245 _aAnalytical solutions for gross thrust change and weight flow ratio due to a jet ejector pump [ Report no. SM- 13881]
_cN.L.Fox
260 _aCalifornia
_bDouglas Aircraft Company
_c1950
300 _a14p
500 _aReport no. SM- 13881
942 _cBK
999 _c560452
_d560452