000 00427 a2200133 4500
001 87800
082 _aPR 177
090 _c41261
_d41261
100 _aMuhammad Amir, NUST Cdt 71008 71 EC
245 _aAeroelastic analysis of reference aircraft wing for investigation of structural stability using Ansys
260 _aRisalpur
_bNUST Risalpur
_c2011
300 _aix,37p.
_eNadeem Sadiq, Sqn Ldr
500 _aBE Project Reports
942 _aCAE NUST
_kPR 177
999 _c322873
_d322873