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NASA NTRS · 19920000026

Program Solves Euler Equations Of Supersonic Flow

Abstract

EMTAC (Euler Marching Technique For Accurate Computation) computer program employs Euler marching algorithm for computing supersonic flows. Enables accurate nonlinear analysis of nonlinear dynamics of supersonic flow over wide range of supersonic mach numbers and angles of attack. Based on exact equations of dynamics of inviscid gas and valid for computations of flows at low and high supersonic mach numbers exhibiting strong shocks and rotational effects. Program also used for inviscid three-dimensional flows fully subsonic or transonic (subsonic with supersonic pockets). Written in FORTRAN V.

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BibTeXRIS

Szema, Kuo-Yen, Chakravarthy, Sukumar, Shankar, Vijaya. 1992-01-01. Program Solves Euler Equations Of Supersonic Flow. https://ntrs.nasa.gov/citations/19920000026

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