Direct calculation method for supersonic inviscid flow around axisymmetric blunt body with conically reentrant afterbody flying at large angle of attac
A numerical method for solving the parabolic approximation to the steady-state compressible Navier-S...
The three-dimensional flow field around blunted bodies traveling at supersonic speed is computed usi...
A time dependent, two dimensional Navier-Stokes code employing the method of body fitted coordinate ...
Hypersonic and supersonic angle of attack flow about asymmetric and axisymmetric blunt bodies based ...
Numerical methods and computer programs for two-dimensional and axisymmetric supersonic flow over bl...
Numerical solutions for blunt axisymmetric bodies in supersonic spherical source flo
Supersonic inviscid flow of equilibrium real gas over blunt axisymmetric bodies at large angles of a...
Application of a general method for calculation of inviscid hypersonic flow fields is discussed. Gen...
Flow fields about axisymmetric blunt bodies at large angles of attack calculated by IBM 7094 compute...
Time-dependant method for calculating supersonic blunt body flow fields with sharp corners and embed...
Linearized characteristics method, and equivalent body method for predicting flow field about axisym...
Numerical analysis of free flow fields around axisymmetric blunt bodies in supersonic fligh
A formulation of the complete Navier-Stokes problem for a viscous hypersonic flow in general curvili...
Three dimensional inviscid flow field analysis for axisymmetric configurations at angle of attac
Comparisons with experimental data and the results of other computational methods demonstrated that ...
A numerical method for solving the parabolic approximation to the steady-state compressible Navier-S...
The three-dimensional flow field around blunted bodies traveling at supersonic speed is computed usi...
A time dependent, two dimensional Navier-Stokes code employing the method of body fitted coordinate ...
Hypersonic and supersonic angle of attack flow about asymmetric and axisymmetric blunt bodies based ...
Numerical methods and computer programs for two-dimensional and axisymmetric supersonic flow over bl...
Numerical solutions for blunt axisymmetric bodies in supersonic spherical source flo
Supersonic inviscid flow of equilibrium real gas over blunt axisymmetric bodies at large angles of a...
Application of a general method for calculation of inviscid hypersonic flow fields is discussed. Gen...
Flow fields about axisymmetric blunt bodies at large angles of attack calculated by IBM 7094 compute...
Time-dependant method for calculating supersonic blunt body flow fields with sharp corners and embed...
Linearized characteristics method, and equivalent body method for predicting flow field about axisym...
Numerical analysis of free flow fields around axisymmetric blunt bodies in supersonic fligh
A formulation of the complete Navier-Stokes problem for a viscous hypersonic flow in general curvili...
Three dimensional inviscid flow field analysis for axisymmetric configurations at angle of attac
Comparisons with experimental data and the results of other computational methods demonstrated that ...
A numerical method for solving the parabolic approximation to the steady-state compressible Navier-S...
The three-dimensional flow field around blunted bodies traveling at supersonic speed is computed usi...
A time dependent, two dimensional Navier-Stokes code employing the method of body fitted coordinate ...