Ali Javed <br/><br/>
To Find out the effects of Pitch rate, Reynolds number and Thickness on the dynamic stall of a Pitching Airfoil  CAEG-53 (A) 
Hossein Raza Hamdani 
 - 1st 
 - Risalpur  NUST  2001 
 - 82p 
<br/><br/> BE-Project Report 
<br/><br/><label>Dewey Class. No.: </label>PR-515