A numerical method is developed to analyze the inviscid flowfield of a high speed inlet by the solution of the Euler equations. The lower-upper implicit scheme in conjunction with adaptive dissipation proves to be an efficient and robust nonoscillatory shock capturing technique for high Mach number flows as well as for transonic flows.
An LU implicity scheme for high speed inlet analysis
Joint Propulsion Conference ; 1986 ; Huntsville, AL, United States
1986-04-01
Report
No indication
English
An LU implicit scheme for high speed inlet analysis
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