Direct Numerical Simulation of roughness-induced transition in the boundary layer of a hypersonic spherical forebody under considertation of high-temperature gas effects
Document type:
Konferenzbeitrag
Contribution type:
Textbeitrag / Aufsatz
Author(s):
Di Giovanni, A.; Stemmer, C.
Keywords:
Direct Numerical Simulation; roughness-induced transition; boundary layer; hypersonic spherical forebody; High-temperature gas effects