Numerical simulation of sonic boom near-field flow over 69-degree delta wing body

T. Kiseleva, S. Lukeshevich

Research output: Contribution to journalConference articlepeer-review

Abstract

Fast and accurate prediction of sonic boom intensity is important in performing design and optimization studies of a supersonic aircraft. The paper presents the computational mesh generation technique for sonic boom prediction in the near field of complex geometry body. Studies are done on a 69-degree delta wing body model used for testing various prediction techniques in the framework of the AIAA Sonic Boom Prediction Workshops.

Original languageEnglish
Article number012111
JournalJournal of Physics: Conference Series
Volume1404
Issue number1
DOIs
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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