Add to ORKGComputer program for determining inviscid flow around blunt bodies at supersonic and hypersonic speeds - users manua
Research in aerodynamics is discussed. The development of equilibrium air curve fits; computation of...
A comprehensive computational procedure is presented for predicting the supersonic region of the flo...
Numerical calculation of inviscid adiabatic flow field around blunt bodies at hypersonic speed
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...
A numerical procedure has been developed to compute the inviscid super/hypersonic flow field about c...
Flow fields about axisymmetric blunt bodies at large angles of attack calculated by IBM 7094 compute...
Hypersonic and supersonic angle of attack flow about asymmetric and axisymmetric blunt bodies based ...
The use of a computer code for the calculation of steady, supersonic, three dimensional, inviscid fl...
A numerical procedure was developed to compute the inviscid super/hypersonic flow field about comple...
At the Fifth Space Congress, a method was [ presented for predicting the inviscid gas properties sur...
A description of the computer program used for heating rate calculation for blunt bodies in hyperson...
Computer program for determining radiating nonadiabatic inviscid flow over blunt body by integral eq...
Time-dependant method for calculating supersonic blunt body flow fields with sharp corners and embed...
Supersonic inviscid flow of equilibrium real gas over blunt axisymmetric bodies at large angles of a...
Research in aerodynamics is discussed. The development of equilibrium air curve fits; computation of...
A comprehensive computational procedure is presented for predicting the supersonic region of the flo...
Numerical calculation of inviscid adiabatic flow field around blunt bodies at hypersonic speed
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...
A numerical procedure has been developed to compute the inviscid super/hypersonic flow field about c...
Flow fields about axisymmetric blunt bodies at large angles of attack calculated by IBM 7094 compute...
Hypersonic and supersonic angle of attack flow about asymmetric and axisymmetric blunt bodies based ...
The use of a computer code for the calculation of steady, supersonic, three dimensional, inviscid fl...
A numerical procedure was developed to compute the inviscid super/hypersonic flow field about comple...
At the Fifth Space Congress, a method was [ presented for predicting the inviscid gas properties sur...
A description of the computer program used for heating rate calculation for blunt bodies in hyperson...
Computer program for determining radiating nonadiabatic inviscid flow over blunt body by integral eq...
Time-dependant method for calculating supersonic blunt body flow fields with sharp corners and embed...
Supersonic inviscid flow of equilibrium real gas over blunt axisymmetric bodies at large angles of a...
Research in aerodynamics is discussed. The development of equilibrium air curve fits; computation of...
A comprehensive computational procedure is presented for predicting the supersonic region of the flo...
Numerical calculation of inviscid adiabatic flow field around blunt bodies at hypersonic speed