Global ETD Search

Search theses and dissertations gathered from participating repositories worldwide. Every result links back to the library that holds it. No account is needed.

Results

Showing 1 to 6 of 6 for “"compressible turbulence"”.

  1. Numerical method for compressible turbulence with shock waves

    wichita-thes

  2. Compressible turbulence in a high-speed high Reynolds number mixing layer

    Compressible turbulence in a high-speed, high Reynolds number, supersonic free shear layer was studied. A two-dimensional free mixing layer was chosen to study turbulence rather than a wall bounded flow due to the experimental fact that the effects of compressibility become significant at lower …

    vt Repository record for Compressible turbulence in a high-speed high Reynolds number mixing layer (opens in a new tab)

  3. A discontinuous Galerkin spectral element method compressible flow solver

    … algorithms for highly-scalable high-order compressible flow simulation using the discontinuous Galerkin spectral element method. The algorithms are designed for simulation of compressible turbulence in realistic engineering geometries that are relevant to a broad range of mechanical …

    uiuc Repository record for A discontinuous Galerkin spectral element method compressible flow solver (opens in a new tab)

  4. An exact and consistent adjoint method for high-fidelity discretization of the compressible flow equations

    … have enabled accurate predictions of complex compressible turbulence phenomena, such as the generation of jet noise that motivates the present effort. However, limited understanding of underlying physical mechanisms restricts the utility of such predictions since they do not, by themselves, …

    uiuc Repository record for An exact and consistent adjoint method for high-fidelity discretization of the compressible flow equations (opens in a new tab)

  5. Three-dimensional turbulence mechanisms in a supersonic separated/reattaching longitudinal cylinder wake

    … work provides a detailed characterization of the turbulence structure in the near-wake of a blunt-based cylinder aligned at zero angle-of-attack in a Mach 2.49 freestream. Particular emphasis is placed in this work on the identification of turbulence mechanisms in the flow regions both upstream …

    uiuc Repository record for Three-dimensional turbulence mechanisms in a supersonic separated/reattaching longitudinal cylinder wake (opens in a new tab)

  6. Aerothermal and aeroelastic response prediction of aerospace structures in high-speed flows using direct numerical simulation

    … the National Aerospace Plane. In this work, the compressible Navier-Stokes equations for a thermally perfect gas and the transient heat equation in the structure are solved simultaneously using two high-fidelity solvers coupled at the solid-fluid interface. Predicted surface heat fluxes are …

    uiuc Repository record for Aerothermal and aeroelastic response prediction of aerospace structures in high-speed flows using direct numerical simulation (opens in a new tab)