NASA NTRS · 19740034220
A relaxation method for calculating transonic flows with detached bow shocks
Abstract
The use of Murman and Krupp's (1971) method for calculating steady, inviscid, transonic flows with imbedded shock waves is discussed in application to two-dimensional problems for transonic flows past sharp and moderately blunt nosed geometries. A relaxation algorithm is used to solve the equations.
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Murman, E. M.. 1973-01-01. A relaxation method for calculating transonic flows with detached bow shocks. https://ntrs.nasa.gov/citations/19740034220
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