000 00471 a2200145 4500
001 88338
082 _aPR-577
090 _c41758
_d41758
100 _aSameer Ahmed
245 _aNeuro Computation based inverse problem of Airfoil Geometry determination; satisfying pre-stated specifications of lift and drag with varing angles of attack
_cAthar Kharal
_pCAEG-56 (A)
250 _a1st
260 _aRisalpur
_bNUST
_c2002
300 _a109p
500 _aBE Project Report
942 _aCAE NUST
_kPR-577
999 _c323411
_d323411