Subsonic flow over a thin airfoil in ground effect

  • Mohamed Serry American University of Sharjah
  • Amjad Tuffaha American University of Sharjah

Abstract




In this paper, the problem of compressible flow over a thin airfoil located near the ground is studied. A singular integral equation, also known as Possio equation, that relates the pressure jump along the airfoil to its downwash is derived. The derivation of the equation utilizes Laplace transform, Fourier transform, method of images, and theory of Mikhlin multipliers. The existence and uniqueness of solution to the Possio equation is verified for the steady state case and an approximate solution is obtained. The aerodynamic loads are then calculated based on the approximate solution. Moreover, the divergence speed of a continuum wing structure located near the ground is obtained based on the derived expressions for the aerodynamic loads.




Published
Nov 26, 2017
How to Cite
SERRY, Mohamed; TUFFAHA, Amjad. Subsonic flow over a thin airfoil in ground effect. Nonlinear Studies, [S.l.], v. 24, n. 4, p. 883-901, nov. 2017. ISSN 2153-4373. Available at: <http://nonlinearstudies.com/index.php/nonlinear/article/view/1454>. Date accessed: 15 dec. 2017.