| 000 | 00357 a2200133 4500 | ||
|---|---|---|---|
| 001 | 89106 | ||
| 082 | _aPR 833 | ||
| 090 |
_c42054 _d42054 |
||
| 100 | _aAdil Jalil | ||
| 245 | _aTo evaluate the aerodynamic parameters of wing and vertical tail by finite element technique | ||
| 260 |
_aKarachi _bNED _c1983 |
||
| 300 | _a216p. | ||
| 500 | _aBE Project Reports | ||
| 942 |
_aCAE NUST _kPR 833 |
||
| 999 |
_c324179 _d324179 |
||