The use of high-order composite compact schemes for computing supersonic jet interaction with a surface
From MaRDI portal
Publication:5413228
DOI10.1134/S0965542513080101zbMath1299.76126MaRDI QIDQ5413228
Publication date: 28 April 2014
Published in: Computational Mathematics and Mathematical Physics (Search for Journal in Brave)
high-order composite compact schemesjet interaction with a flat surfacestrong discontinuities of flowsupersonic axisymmetric jet
Cites Work
- A shock-capturing methodology based on adaptative spatial filtering for high-order non-linear computations
- Compact finite difference schemes with spectral-like resolution
- A family of low dispersive and low dissipative explicit schemes for flow and noise computations.
- Multioperator schemes of arbitrary order based on noncentered compact approximations
- On the use of higher-order finite-difference schemes on curvilinear and deforming meshes
- Monotone compact running schemes for systems of hyperbolic equations
- Implicit Finite-Difference Simulation of Flow about Arbitrary Two-Dimensional Geometries
- Oscillations of a moderately underexpanded choked jet impinging upon a flat plate
- Flow field and noise characteristics of a supersonic impinging jet
- Hybrid schemes with high-order multioperators for computing discontinuous solutions
- An experimental study of the oscillatory flow structure of tone-producing supersonic impinging jets
- High-order composite compact schemes for simulation of viscous gas flows
- On the structure of internal dissipation of composite compact schemes for gasdynamic simulation
- Unnamed Item
- Unnamed Item
- Unnamed Item
- Unnamed Item
This page was built for publication: The use of high-order composite compact schemes for computing supersonic jet interaction with a surface