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for Transonic and Separated Flows About Airfoils

Leland A. Carlson

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Abstract

A DIRECT-INVERSE METHOD FOR TRANSONIC AND SEPARATEDFLOWS ABOUT AIRFOILSLeland A. CarlsonAerospace Engineering DepartmentTexas AM and it is formulated using Cartesian coordinates. Since the methodutilizes inverse boundary conditions in regions of separated flow, it issuitable for predicting the flowfield about airfoils having trailing edgeseparated flow under high lift conditions. Comparisons with experimental dataindicate that the method should be a useful tool for applied aerodynamicanalyses.

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What this paper is about

A DIRECT-INVERSE METHOD FOR TRANSONIC AND SEPARATEDFLOWS ABOUT AIRFOILSLeland A. CarlsonAerospace Engineering DepartmentTexas AM and it is formulated using Cartesian coordinates. Since the methodutilizes inverse boundary conditions in regions of separated flow, it issuitable for predicting the flowfield about airfoils having trailing edgeseparated flow under high lift conditions. Comparisons with experimental dataindicate that the method should be a useful tool for applied aerodynamicanalyses.

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Available abstract

A DIRECT-INVERSE METHOD FOR TRANSONIC AND SEPARATEDFLOWS ABOUT AIRFOILSLeland A. CarlsonAerospace Engineering DepartmentTexas AM and it is formulated using Cartesian coordinates. Since the methodutilizes inverse boundary conditions in regions of separated flow, it issuitable for predicting the flowfield about airfoils having trailing edgeseparated flow under high lift conditions. Comparisons with experimental dataindicate that the method should be a useful tool for applied aerodynamicanalyses.

Key concepts: Transonic, Airfoil, Lift coefficient, Mechanics, Inverse, Mathematics, Lift (data mining), Aerodynamics

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