| 000 | 00629 a2200241 4500 | ||
|---|---|---|---|
| 001 | 306894 | ||
| 020 | _a | ||
| 041 | _aeng | ||
| 080 | _aLNASA TN D-7976 : 1975 | ||
| 245 | _aExperimental and numerical investigation of boundary-layer development and transition on the walls of a mach 5 nozzle | ||
| 250 | _a | ||
| 260 | _aWashington, D.C. | ||
| 260 | _bNASA | ||
| 260 | _c1975 | ||
| 300 | _a86 p. | ||
| 300 | _c | ||
| 856 | _uNASA | ||
| 490 | _aNASA TN D-7976 : 1975 | ||
| 700 | _a | ||
| 650 | _a | ||
| 650 | _aBoundary-layer stability & transition, Nozzle and channel flow, Supersonic and hypersonic flow | ||
| 942 | _cPP | ||
| 942 | _2UDC | ||
| 999 |
_c255066 _d255066 |
||