Decoupled implicit method for aerothermodynamics and reacting flows

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Abstract

We propose a new implicit computational fluid dynamics method for steady-state compressible reacting flows. The concept is to decouple the total mass, momentum, and energy conservation equations from the species mass and internal energy equations and to solve the two equation sets sequentially. With certain approximations to the implicit system, it is possible to dramatically reduce the cost of the solution with little to no penalty on the convergence properties. Importantly, the cost of the decoupled implicit problem scales linearly with the number of species, as opposed to the quadratic scaling for the conventional fully coupled method. Furthermore, the new approach reduces the memory requirements by a significant factor. The decoupled implicit method shows promise for the application to aerothermodynamics problems and reacting flows.

Original languageEnglish (US)
Pages (from-to)1245-1254
Number of pages10
JournalAIAA journal
Volume51
Issue number5
DOIs
StatePublished - May 2013

Bibliographical note

Funding Information:
This work was sponsored by the Air Force Research Laboratory under grant FA9453-12-1-0133, the Air Force Office of Scientific Research under grant FA9550-10-1-0563, and by the Department of Defense National Security Science and Engineering Faculty Fellowship. The views and conclusions contained herein are those of the author and should not be interpreted as necessarily representing the official policies or endorsements, either expressed or implied, of the sponsors or the U.S. Government.

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