| 000 | 00687 a2200241 4500 | ||
|---|---|---|---|
| 001 | 256067 | ||
| 020 | _a | ||
| 041 | _aeng | ||
| 080 | _aLNASA CR 4651 : 1995 | ||
| 245 | _aEuler technology assessment for preliminary aircraft design employing overflow code with muliblock structured-grid method | ||
| 250 | _a | ||
| 260 | _aWashington, D.C. | ||
| 260 | _bNational Aeronautics and Space Adminstration | ||
| 260 | _c1995 | ||
| 300 | _a66 p. | ||
| 300 | _c | ||
| 856 | _u | ||
| 490 | _aNASA CR 4651 : 1995 | ||
| 700 | _a | ||
| 650 | _a | ||
| 650 | _aComputational fluid dynamics, Euler formulation,Preliminary aircraft design, Sharp-edge flow-separation, Vortex flow | ||
| 942 | _cPP | ||
| 942 | _2UDC | ||
| 999 |
_c207201 _d207201 |
||