Flow control for oblique shock wave reflections

Doctoral thesis English OPEN
Giepman, R.H.M.;
  • Subject:
    arxiv: Physics::Fluid Dynamics

Shock wave-boundary layer interactions are prevalent in many aerospace applications that involve transonic or supersonic flows. Such interactions may lead to boundary layer separation, flow unsteadiness and substantial losses in the total pressure. Flow control techniqu... View more
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