Sameer Ahmed <br/><br/>
Neuro Computation based inverse problem of Airfoil Geometry determination; satisfying pre-stated specifications of lift and drag with varing angles of attack  CAEG-56 (A) 
Athar Kharal 
 - 1st 
 - Risalpur  NUST  2002 
 - 109p 
<br/><br/> BE Project Report 
<br/><br/><label>Dewey Class. No.: </label>PR-577