Add to ORKGA general method developed for the analysis of inviscid hypersonic shock layers is discussed for app...
Application of a general method for calculation of inviscid hypersonic flow fields is discussed. Gen...
Pressure distributions, aerodynamic coefficients, and shock shapes were measured on blunt bodies of ...
Supersonic inviscid flow of equilibrium real gas over blunt axisymmetric bodies at large angles of a...
Direct calculation method for supersonic inviscid flow around axisymmetric blunt body with conically...
Flow field analysis over blunt axisymmetric body in perfect gas or equilibrium air using method of i...
Computer program for determining inviscid flow around blunt bodies at supersonic and hypersonic spee...
This paper describes two computer programs which have been combined to obtain inviscid perfect and r...
Numerical methods and computer programs for two-dimensional and axisymmetric supersonic flow over bl...
Hypersonic and supersonic angle of attack flow about asymmetric and axisymmetric blunt bodies based ...
Entropy layer surrounding three dimensional blunt body at angle of attack determined in wind tunnel ...
Three dimensional inviscid flow field analysis for axisymmetric configurations at angle of attac
Linearized characteristics method, and equivalent body method for predicting flow field about axisym...
Pressure distributions for blunt body wind tunnel models at supersonic speeds and angles of attack f...
The goal of this research is the assessment of the validity of existing three dimensional numerical ...
A general method developed for the analysis of inviscid hypersonic shock layers is discussed for app...
Application of a general method for calculation of inviscid hypersonic flow fields is discussed. Gen...
Pressure distributions, aerodynamic coefficients, and shock shapes were measured on blunt bodies of ...
Supersonic inviscid flow of equilibrium real gas over blunt axisymmetric bodies at large angles of a...
Direct calculation method for supersonic inviscid flow around axisymmetric blunt body with conically...
Flow field analysis over blunt axisymmetric body in perfect gas or equilibrium air using method of i...
Computer program for determining inviscid flow around blunt bodies at supersonic and hypersonic spee...
This paper describes two computer programs which have been combined to obtain inviscid perfect and r...
Numerical methods and computer programs for two-dimensional and axisymmetric supersonic flow over bl...
Hypersonic and supersonic angle of attack flow about asymmetric and axisymmetric blunt bodies based ...
Entropy layer surrounding three dimensional blunt body at angle of attack determined in wind tunnel ...
Three dimensional inviscid flow field analysis for axisymmetric configurations at angle of attac
Linearized characteristics method, and equivalent body method for predicting flow field about axisym...
Pressure distributions for blunt body wind tunnel models at supersonic speeds and angles of attack f...
The goal of this research is the assessment of the validity of existing three dimensional numerical ...
A general method developed for the analysis of inviscid hypersonic shock layers is discussed for app...
Application of a general method for calculation of inviscid hypersonic flow fields is discussed. Gen...
Pressure distributions, aerodynamic coefficients, and shock shapes were measured on blunt bodies of ...