Wind Tunnel Investigation of Pressure Distribution and Transition Position of a Swept 3D Wing

Mohammad Reza Dr. Soltani; M. Masdari; M. Seidjafari; Kaveh Ghorbanian

Volume 7, Issue 2 , September 2010, , Pages 132-137

Abstract
  Extensive wind tunnel tests are conducted to evaluate surface pressure distribution of a semi span swept wing. The wing section has a laminar flow airfoil similar to NACA 6-series airfoils. The investigations are conducted at various speeds and angles of attack. Surface pressure distribution over the ...  Read More