Saifur Rehman Bakaul <br/><br/>
To Investigate the Effect of Reynolds number, Oscillation rate, Thickness Ratio and Pivot point position on Dynamic stall of an Oscillating Airfoil  CAEG-53 (A) 
Hussein Raza Hamdani 
 - 1st 
 - Risalpur  NUST  2001 
 - 98p 
<br/><br/> BE- Project Report 
<br/><br/><label>Dewey Class. No.: </label>PR-516