000 00421 a2200145 4500
001 88311
082 _aPR 508
090 _c41731
_d41731
100 _aFahad Memon
245 _aTo Study the effect of Reynolds number and Thickness Ratio on Aerodynamic Performance of an Airfoil
_cHossein Raza Hamdhani
_pCAEG-53 (A)
250 _a1st
260 _aRisalpur
_bNUST
_c2001
300 _a52p
500 _aBE Project Reports
942 _aCAE NUST
_kPR 508
999 _c323384
_d323384