Direct Numerical Simulation of roughness-induced transition in the boundary layer of a hypersonic spherical forebody under considertation of high-temperature gas effects
Dokumenttyp:
Konferenzbeitrag
Art des Konferenzbeitrags:
Textbeitrag / Aufsatz
Autor(en):
Di Giovanni, A.; Stemmer, C.
Stichworte:
Direct Numerical Simulation; roughness-induced transition; boundary layer; hypersonic spherical forebody; High-temperature gas effects