A time-dependent computational method for blunt body flows.
From MaRDI portal
Publication:5522875
DOI10.2514/3.3867zbMath0145.46402OpenAlexW2992905873MaRDI QIDQ5522875
Publication date: 1966
Published in: AIAA Journal (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.2514/3.3867
Related Items (36)
An unstructured, three-dimensional, shock-fitting solver for hypersonic flows ⋮ A novel stabilization method for high-order shock fitting with finite element methods ⋮ Selected topics in the theory and practice of computational fluid dynamics ⋮ Implications of truncating semi-infinite physical domains on the accuracy of the solutions to the N-S equations ⋮ On high-order shock-fitting and front-tracking schemes for numerical simulation of shock-disturbance interactions ⋮ Natural convection in a cavity with a sloping upper surface filled with an anisotropic porous material ⋮ Application of a shock-fitted spectral collocation method for computing transient high-speed inviscid flows over a blunt nose ⋮ Standardized pseudospectral formulation of the inviscid supersonic blunt body problem ⋮ Heuristical and numerical considerations for the carbuncle phenomenon ⋮ A shock-fitting technique for cell-centered finite volume methods on unstructured dynamic meshes ⋮ Computation of weak steady shock reflections by means of an unstructured shock-fitting solver ⋮ On problems associated with grid convergence of functionals ⋮ A mapping technique for numerical computations of bed evolutions ⋮ A new shock-capturing technique based on moving least squares for higher-order numerical schemes on unstructured grids ⋮ An embedded shock-fitting technique on unstructured dynamic grids ⋮ Numerical simulation of shock/boundary-layer interaction using an unstructured shock-fitting technique ⋮ Very-high-order TENO schemes with adaptive accuracy order and adaptive dissipation control ⋮ Entropy layers ⋮ An evaluation of cell type finite difference methods for solving viscous flow problems ⋮ Convergence acceleration for high-order shock-fitting methods in hypersonic flow applications with efficient implicit time-stepping schemes ⋮ Computation of three dimensional flows about aircraft configurations ⋮ Generalized nonlinear minimal residual (GNLMR) method for iterative algorithms ⋮ On the application of boundary conditions to time dependent computations for quasi one-dimensional fluid flows ⋮ Coefficient matrices for implicit finite difference solution of the inviscid fluid conservation law equations ⋮ Study of the flow of fluids and gases ⋮ Second-order curved shock theory ⋮ A Brief History of Shock-Fitting ⋮ Application of the unsteady numerical method of Godunov to computation of supersonic flows past bell-shaped bodies ⋮ Analytic model of a resistive magnetohydrodynamic shock without Hall effect ⋮ Calculation of supersonic flow around V-shaped wings by the fitting method ⋮ An open boundary condition for the computation of the steady incompressible Navier-Stokes equations ⋮ On artificial viscosity ⋮ Shock-fitted multidomain solution of supersonic flows ⋮ Calculation of three-dimensional transonic gas flow through a stage of an axial turbine ⋮ Thirty-six years of shock fitting. ⋮ Implicit and semi-implicit well-balanced finite-volume methods for systems of balance laws
This page was built for publication: A time-dependent computational method for blunt body flows.
