Separation flow control by thermal bump in a supersonic airflow
Joint Institute of High Temperature of the Russian Academy of Sciences - 125412, Izhorskaya str. 13/2, Moscow, Russian Federation and Moscow Institute of Physics and Technology - 141700, Insitytsky per. 9, Dolgoprudny, Moscow Region, Russian Federation
Received: 31 March 2012
Accepted: 13 June 2012
This paper presents a numerical and theoretical investigation of a flow separation control by a thermal bump (spark discharge) in Mach M = 2 flow over a profile NACA64a212.
PACS: 52.80.Tn – Other gas discharges / 47.65.Md – Plasma dynamos
© EPLA, 2012