When the differential equations describing the flow of compressible fluids are derived under the assumptions that (1) forces in the fluid are due only to variations in pressure and (2) that the entropy of any volume element remains constant, it can be shown mathematically that these differential equations cannot have continuous solutions under all circumstances. If we adopt the notion of “shock discontinuities” in these solutions, the differential equations describing the flow in continuous regions together with conditions expressing the laws of conservation across the discontinuities suffice to completely determine the flow. An alternative procedure is to use a method, develop recently by J. Von Neumann and R. D. Richtmyer [3], which intro...
AbstractIn order to investigate the linearized stability or instability of compressible flows, as it...
One of the most important and complex effects in compressible fluid flow simulation is a shock-captu...
Thesis: S.M., Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, 201...
A wide class of difference equations is described for approximating discontinuous time dependent sol...
A method for automatically taking into account the shock discontinuities in the flow problems whenev...
Physical discontinuities, such as shocks and interfaces occur commonly in fluid mechanics. The empha...
Models C and D are mathematical formulations for the motion of materials. Model C is the classical, ...
tion into the numerical procedure for integration of conservative equations of gas dynamics, allowin...
This report describes a numerical method to calculate the flow of a compressible fluid in the presen...
The physical behavior of compressible fluid flow is quite different from incompressible fluid flow. ...
The investigation of Mach reflection formed after the impingement of a weak plane shock wave on a we...
On the example of the Navier-Stokes model, this paper discusses the approach in which the surface of...
It is shown that on non-shock regions the difference equations of von Neumann and Richtmyer for one-...
This thesis consists of an introduction and five papers concerning different numerical and mathemati...
"Contract W-7405-ENG.36 with the U.S. Atomic Energy Commission."--Cover."Report written: May 1955; R...
AbstractIn order to investigate the linearized stability or instability of compressible flows, as it...
One of the most important and complex effects in compressible fluid flow simulation is a shock-captu...
Thesis: S.M., Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, 201...
A wide class of difference equations is described for approximating discontinuous time dependent sol...
A method for automatically taking into account the shock discontinuities in the flow problems whenev...
Physical discontinuities, such as shocks and interfaces occur commonly in fluid mechanics. The empha...
Models C and D are mathematical formulations for the motion of materials. Model C is the classical, ...
tion into the numerical procedure for integration of conservative equations of gas dynamics, allowin...
This report describes a numerical method to calculate the flow of a compressible fluid in the presen...
The physical behavior of compressible fluid flow is quite different from incompressible fluid flow. ...
The investigation of Mach reflection formed after the impingement of a weak plane shock wave on a we...
On the example of the Navier-Stokes model, this paper discusses the approach in which the surface of...
It is shown that on non-shock regions the difference equations of von Neumann and Richtmyer for one-...
This thesis consists of an introduction and five papers concerning different numerical and mathemati...
"Contract W-7405-ENG.36 with the U.S. Atomic Energy Commission."--Cover."Report written: May 1955; R...
AbstractIn order to investigate the linearized stability or instability of compressible flows, as it...
One of the most important and complex effects in compressible fluid flow simulation is a shock-captu...
Thesis: S.M., Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, 201...