Archivio Istituzionale della RicercaA numerical technique to solve the Euler equa- tions for two-dimensional, steady, inviscid, supersonic flows in ducts is presented. The technique is second-order accurate and is based on the A-scheme plus shock-fitting method. Many cases have been tested. The method u s e dand t h ere- sults obtained demonstrate the versatility of the technique specially if confronted with analogous methods that use shock-capturing techniques
Shock-Fitting Method for Two-Dimensional Inviscid, Steady SupersonicFlows in Ducts / Marsilio, Roberto; Moretti, G.. - In: MECCANICA. - ISSN 0025-6455. - ELETTRONICO. - 24:(1989), pp. 216-222. [10.1007/BF01556453]
Shock-Fitting Method for Two-Dimensional Inviscid, Steady SupersonicFlows in Ducts
MARSILIO, Roberto;
1989
Abstract
A numerical technique to solve the Euler equa- tions for two-dimensional, steady, inviscid, supersonic flows in ducts is presented. The technique is second-order accurate and is based on the A-scheme plus shock-fitting method. Many cases have been tested. The method u s e dand t h ere- sults obtained demonstrate the versatility of the technique specially if confronted with analogous methods that use shock-capturing techniques
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https://hdl.handle.net/11583/1403082