Computational grid adaptation for the sonic boom near field modeling

T. Kiseleva, V. Temerbekov

Research output: Contribution to journalConference articlepeer-review


This paper discusses the numerical simulation of the 69-Degree Delta Wing Body for computing the sonic boom signature in the near field. For flow field calculation, the commercial CFD flow solver ANSYS Fluent is employed. The computational mesh in the perturbed flow regions was refined two times using the automatic gradient adaptation. The results are in agreement with the results obtained by other researchers.

Original languageEnglish
Article number012112
JournalJournal of Physics: Conference Series
Issue number1
Publication statusPublished - 6 Dec 2019
Event16th All-Russian Seminar with International Participation on Dynamics of Multiphase Media, DMM 2019 - Novosibirsk, Russian Federation
Duration: 30 Sep 20195 Oct 2019


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