Gas turbines are, and will continue to be, the backbone of narrow and wide body aircraft
propulsion. The main reason for the success of gas turbines is their power density, ie thrust …

The spectral analysis is a basic tool to characterise the behaviour of any convection scheme.
By nature, the solution projected onto the Fourier basis enables to estimate the dissipation …

In the present paper, a stable Spectral Difference formulation on triangles is defined using a
flux polynomial expressed in the Raviart-Thomas basis up to the sixth-order of accuracy …

An approach for modeling time-domain impedance boundary conditions (TDIBC) is
presented. Its implementation in numerical codes relies on the inverse Fourier transform to …

Some possible future High Fidelity CFD codes for LES simulation of turbomachinery are
compared on several test cases increasing in complexity, starting from a very simple inviscid …

A computational fluid dynamics code is differentiated using algorithmic differentiation (AD) in
both tangent and adjoint modes. The two novelties of the present approach are (1) the …

The attenuation power of an acoustic liner is optimized by unsteady compressible flow
simulations that model the presence of the liner with a time-domain impedance boundary …

This work deals with high-order numerical methods for unsteady flows around complex
geometries. In order to cope with the low-order industrial Finite Volume Method, the …

The natural transition of hypersonic boundary layers (HBLs) is often expressed in terms of
discrete modes and their linear stability. A frequent interpretation revolves around fast and …

A Spectral Difference (SD) algorithm on tensor-product elements which solves the reacting
compressible Navier-Stokes equations (NSE) is presented. The classical SD algorithm is …