Nauman Ahmed; Prof Shakeel (Advisor) <br/><br/>
Determination of Velocity Profile for the improvement of Flow Quality of CAE 2x3 Subsonic Wind Tunnel. (2) To facilitate the Yawing motion of an aircraft model in the wind tunnel by fabricating and installing a rotating plateform and directional stability test of F-6 and F-7P AIRCRAFT MODELS   44 "A" EC 

 - Karachi  NED University  1996 
 - 73p 
<br/><br/> BE Project Reports 
<br/><br/><label>Dewey Class. No.: </label>PR 1224