Add to ORKGFinite difference method of solving normal shock wave-sphere interaction problem for ideal and real gas flow field
A Lagrangian method is developed to solve the Euler equations of gas dynamics. The solution of the e...
A time dependent finite difference method used to calculate blunt body flows with impinging shock is...
A time-marching finite-difference method was used to solve the compressible Navier-Stokes equations ...
Finite difference method to obtain numerical results on normal shock wave diffraction by sphere and ...
A method for determining shock-wave shapes, stagnation-point location, and flow-field properties for...
Finite difference method for unsteady flows applied to steady state equations for supersonic region ...
Two-dimensional axisymmetric, reacting viscous flow over blunt projectiles is computed to study shoc...
A finite difference scheme with a shock-fitting algorithm has been used to investigate unsteady invi...
Nonintrusive measurements were made of a normal shock wave/boundary layer interaction. Two dimension...
The two dimensional, time dependent Euler equations which govern the flow field resulting from the i...
Two-dimensional and three-dimensional computational fluid dynamics studies of a spherical bubble imp...
Pressure distributions, aerodynamic coefficients, and shock shapes were measured on blunt bodies of ...
Time-dependant method for calculating supersonic blunt body flow fields with sharp corners and embed...
Numerical analysis of free flow fields around axisymmetric blunt bodies in supersonic fligh
Measured shock shapes are presented for sphere and hemisphere models in helium, air, CF4, C2F6, and ...
A Lagrangian method is developed to solve the Euler equations of gas dynamics. The solution of the e...
A time dependent finite difference method used to calculate blunt body flows with impinging shock is...
A time-marching finite-difference method was used to solve the compressible Navier-Stokes equations ...
Finite difference method to obtain numerical results on normal shock wave diffraction by sphere and ...
A method for determining shock-wave shapes, stagnation-point location, and flow-field properties for...
Finite difference method for unsteady flows applied to steady state equations for supersonic region ...
Two-dimensional axisymmetric, reacting viscous flow over blunt projectiles is computed to study shoc...
A finite difference scheme with a shock-fitting algorithm has been used to investigate unsteady invi...
Nonintrusive measurements were made of a normal shock wave/boundary layer interaction. Two dimension...
The two dimensional, time dependent Euler equations which govern the flow field resulting from the i...
Two-dimensional and three-dimensional computational fluid dynamics studies of a spherical bubble imp...
Pressure distributions, aerodynamic coefficients, and shock shapes were measured on blunt bodies of ...
Time-dependant method for calculating supersonic blunt body flow fields with sharp corners and embed...
Numerical analysis of free flow fields around axisymmetric blunt bodies in supersonic fligh
Measured shock shapes are presented for sphere and hemisphere models in helium, air, CF4, C2F6, and ...
A Lagrangian method is developed to solve the Euler equations of gas dynamics. The solution of the e...
A time dependent finite difference method used to calculate blunt body flows with impinging shock is...
A time-marching finite-difference method was used to solve the compressible Navier-Stokes equations ...