000 00606 a2200133 4500
001 91328
082 _aPR 1224
090 _c43443
_d43442
100 _aNauman Ahmed; Prof Shakeel (Advisor)
245 _aDetermination 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
_n44 "A" EC
260 _aKarachi
_bNED University
_c1996
300 _a73p
500 _aBE Project Reports
942 _aCAE NUST
_kPR 1224
999 _c326401
_d326401