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Computation of viscus transonic flow over airfoils comparisons and compilation of results

JP Singh

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Abstract

This report gives a collection of several computations13; made on NACA 0012 and NPL 9615 airfoils using a two- dimensional viscous transonic flow analysis based on Bavitz code. The comparisons with experimental results of NPL and NAL indicate that the computer program can be used as a reliable method to compute two-dimensional viscous transonic flows, except in those cases involving strong shock/extensive flow separation.

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What this paper is about

This report gives a collection of several computations13; made on NACA 0012 and NPL 9615 airfoils using a two- dimensional viscous transonic flow analysis based on Bavitz code. The comparisons with experimental results of NPL and NAL indicate that the computer program can be used as a reliable method to compute two-dimensional viscous transonic flows, except in those cases involving strong shock/extensive flow separation.

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Available abstract

This report gives a collection of several computations13; made on NACA 0012 and NPL 9615 airfoils using a two- dimensional viscous transonic flow analysis based on Bavitz code. The comparisons with experimental results of NPL and NAL indicate that the computer program can be used as a reliable method to compute two-dimensional viscous transonic flows, except in those cases involving strong shock/extensive flow separation.

Key concepts: Transonic, NACA airfoil, Airfoil, Computation, Mechanics, Flow (mathematics), Subsonic and transonic wind tunnel, Shock (circulatory)

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