000 00622pam a2200181a 44500
005 20200806112055.0
008 200806b xxu||||| |||| 00| 0 eng d
040 _cIIT Kanpur
041 _aeng
100 _aBlackwell, James A.
245 1 _aA preliminary study of effects of Reynolds number and boundary layer transition location on shock-induced separation [NASA TN D-5003]
_cJames A. Blackwell
260 _bNASA
_c1969
_aWashington, D.C.
300 _a25p
440 _aNational Aeronautics and Space Administration (NASA)
520 _aNASA technical note D-5003
650 _aReynolds number
942 _cREF
999 _c395907
_d395907