000 | 00613 a2200277 4500 | ||
---|---|---|---|
001 | 113779 | ||
020 | _a0 | ||
041 | _aeng | ||
080 | _a533.6.011.5 Dav | ||
245 | _aLaminar compressible flow past axisymmetric blunt bodies : results of a second-order theory | ||
250 | _a | ||
260 | _aStanford | ||
260 | _bStanford University, | ||
260 | _c1963 | ||
300 | _axiii,135 p. | ||
300 | _c24 cm | ||
490 | _a | ||
100 | _aDavis, Randall Thomas | ||
700 | _a | ||
650 | _a | ||
650 | _aAerodynamics | ||
650 | _aBoundary layer | ||
650 | _aCompressibility | ||
942 | _cBK | ||
942 | _2UDC | ||
999 |
_c33179 _d33179 |