| 000 | 00583 a2200241 4500 | ||
|---|---|---|---|
| 001 | 317211 | ||
| 020 | _a | ||
| 041 | _aeng | ||
| 080 | _aLNASA CR 3243 : 1980 | ||
| 245 | _aTransonic flow field analysis for wing - fuselage configurations | ||
| 250 | _a | ||
| 260 | _aWashington, D.C. | ||
| 260 | _bNASA | ||
| 260 | _c1980 | ||
| 300 | _a158 p. | ||
| 300 | _c | ||
| 856 | _u | ||
| 490 | _aNASA CR 3243 : 1980 | ||
| 700 | _a | ||
| 650 | _a | ||
| 650 | _aTransonic flow,Computational aerodynamics,Flow simulations,Wing-fuselage,Finite difference relaxation scheme | ||
| 942 | _cPP | ||
| 942 | _2UDC | ||
| 999 |
_c264005 _d264005 |
||