AFM, Maison de la Mécanique, 39/41 rue Louis Blanc - 92400 Courbevoie
Abstract
Detached Eddy Simulation of restricted shock
separated (RSS) flow has been performed to understand the physics of complex cap-shock
pattern, which is the key cause of separated flow transition in the rocket nozzles.
High-order shock-capturing numerical schemes are necessary to understand this complex
flow. Hence a fifth order monotonicity preserving weighted essentially non-oscillatory
(MPWENO) scheme is used here for good numerical resolution