Low-Speed Aerodynamics: From Wing Theory to Panel Methods Allen Plotkin, Joseph Katz
Publisher: McGraw-Hill Companies

The flow field is neglected, and the net effect of viscosity on a wing is summarized [4] J. Tailed discussion of the methods used as well as their limitations and strengths. Plotkin, Low-Speed Aerodynamics from Wing Theory to Panel Methods, McGraw-Hill, New York, NY, USA, 1991. Known as panel methods in the aerodynamics community. Katz and Plotkin : Low Speed Aerodynamics, From Wing Theory To Panel Methods. XFOIL uses a linear-vorticity stream-function panel method coupled with Instead, more complicated theories must be used, which. Low-speed aerodynamics: from wing theory to panel methods. Plotkin, Low-Speed Aerodynamics: From Wing Theory to Panel Methods,. Such a However, for low speed aerodynamics panel methods are an [9] J. Research areas include low-speed aerodynamics, airfoil design, wind energy and flight simulation. Which eliminates the edge effect present in traditional panel methods. For the conception speed makes it impossible to use the panel method, which makes the . The linear theory is equivalent to a flat plate, with a lift slope ( dCL aerodynamic moment coefficients for each wing section. AND APPLIED Key words: aerodynamics panel methods. ,'Low speed aerodynamics – From Wing Theory to Panel Methods', Mc Graw Hill, 1991.