Control of Incident Shock Induced Separation at Mach 3.5 using an Array of Steady Micro-Jet Actuators

Control of Incident Shock Induced Separation at Mach 3.5 using an Array of Steady Micro-Jet Actuators

  1. Control of Incident Shock Induced Separation at Mach 3.5 using an Array of Steady Micro-Jet Actuators”, 7 TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS), 2017.


Last updated on : 13-10-2017 06:51:35pm