000 00398 a2200133 4500
001 88103
082 _aPR 342
090 _c41514
_d41514
100 _aZawar A Nawaz, 016018
245 _aModel Analysis of a wing using ANSYS and the effect of wing tip missile on this analysis
260 _aRisalpur
_bNUST Risalpur
_c2004
300 _avi, 47p.
_eZubair Islam, Prof
500 _aBE Project Reports
942 _aCAE NUST
_kPR 342
999 _c323176
_d323176