000 00545 a2200241 4500
001 316039
020 _a
041 _aeng
080 _aLNASA TP - 1497 : 1979
245 _aHybridized method for computing high-reynolds-number hypersonic flow about blunt bodies
250 _a
260 _aWashington, D.C.
260 _bNASA
260 _c1979
300 _a46 p.
300 _c
856 _u
490 _aNASA TP - 1497 : 1979
700 _a
650 _a
650 _aBlunt body, Viscous flows, Finite difference
942 _cPP
942 _2UDC
999 _c263339
_d263339