Computational study of flow in a rocket-based combined cycle (RBCC) engine inlet

DOI10.1016/J.COMPFLUID.2006.01.010zbMath1177.76178OpenAlexW2068924989MaRDI QIDQ1043164

J. Blot

Publication date: 7 December 2009

Published in: Computers and Fluids (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.compfluid.2006.01.010

Mathematics Subject Classification ID

Finite difference methods applied to problems in fluid mechanics (76M20) Supersonic flows (76J20)

Uses Software

• Spalart-Allmaras

Cites Work

• An implicit finite-difference algorithm for hyperbolic systems in conservation-law form
• 3-D Navier-Stokes analysis of crossing glancing shocks/turbulent boundary layer interactions
• Implicit Finite-Difference Simulations of Three-Dimensional Compressible Flow

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