Papers from the 2010 Applied Aerodynamics Conference of the Association AĆ©ronautique et Astronautique de France held in Marseille, France.
Numerical Methods
- Multiblock residual-based compact schemes for the computation of complex turbomachinery flows
- Hybrid upwind splitting scheme by combining the approaches of Roe and AUFS for compressible flow problems
- Compressibility effects on laminar-turbulent boundary layer transition
- Transition prediction in transonic turbine configurations using a correlation-based transport equation model
- Numerical study of shock-turbulent boundary layer interactions with incipient and complete separation
- The structure of turbulence in transonic shock wave/boundary layer interaction
- Application of the passive control of shock wave to the reduction of high-speed impulsive noise
- Overview of activities at the ISL hypersonic shock tunnels
- Side loads and thermal loads in rocket nozzles. Overview of the CNES-ONERA ATAC programme
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