Open AccessNumerical simulation of a hypersonic flow over HB-2 model using UST3D programming code
Author(s) -
Arina Kryuchkova
Publication year - 2019
Publication title -
journal of physics. conference series
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.21
H-Index - 85
eISSN - 1742-6596
pISSN - 1742-6588
DOI - 10.1088/1742-6596/1250/1/012010
Subject(s) - aerodynamics , mach number , code (set theory) , hypersonic speed , computer science , flow (mathematics) , computer simulation , aerospace engineering , aerodynamic heating , computational fluid dynamics , mechanics , physics , simulation , engineering , programming language , heat transfer , set (abstract data type)
Numerical modeling of a flow over HB-2 model using UST3D programming code was carried out. Aerodynamic coefficients dependencies from Mach number and angle of attack were compared to various experimental tests results. Good accordance of the numerical method predictions with empirical data was demonstrated. The numerical simulation has provided an extra UST3D code validation in application to aerodynamic calculations of hypersonic flows.