TY - JOUR
T1 - Numerical simulation of sonic boom near-field flow over 69-degree delta wing body
AU - Kiseleva, T.
AU - Lukeshevich, S.
N1 - Publisher Copyright:
© 2019 IOP Publishing Ltd.
Copyright:
Copyright 2020 Elsevier B.V., All rights reserved.
PY - 2019/12/6
Y1 - 2019/12/6
N2 - 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.
AB - 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.
UR - http://www.scopus.com/inward/record.url?scp=85077814945&partnerID=8YFLogxK
U2 - 10.1088/1742-6596/1404/1/012111
DO - 10.1088/1742-6596/1404/1/012111
M3 - Conference article
AN - SCOPUS:85077814945
VL - 1404
JO - Journal of Physics: Conference Series
JF - Journal of Physics: Conference Series
SN - 1742-6588
IS - 1
M1 - 012111
T2 - 16th All-Russian Seminar with International Participation on Dynamics of Multiphase Media, DMM 2019
Y2 - 30 September 2019 through 5 October 2019
ER -