Add to ORKGThe COMOC finite element fluid mechanics computer program system is applicable to diverse problem classes. The two dimensional aerodynamics sequence was established for solution of the potential and/or viscous and turbulent flowfields associated with subsonic flight of elementary two dimensional isolated airfoils. The sequence is constituted of three specific flowfield options in COMOC for two dimensional flows. These include the potential flow option, the boundary layer option, and the parabolic Navier-Stokes option. By sequencing through these options, it is possible to computationally construct a weak-interaction model of the aerodynamic flowfield. This report is the user's guide to operation of COMOC for the aerodynamics sequence
A two dimensional unsteady Navier-Stokes calculation procedure with specific application to the isol...
The use of a computer code for the calculation of two dimensional inlet flow fields in a supersonic ...
Incompressible potential flow calculations are presented that were corrected for compressibility in ...
A weak interaction solution algorithm was established for aerodynamic flow about an isolated airfoil...
An integrated system of computer programs was developed for the design and analysis of supersonic co...
Computer programs to calculate the incompressible potential flow, corrected for compressibility, in ...
An order-of-magnitude analysis of the subsonic three dimensional steady time averaged Navier-Stokes ...
Papers given at the conference present the results of theoretical research on aerodynamic flow probl...
An aerodynamic analysis system based on potential theory at subsonic and/or supersonic speeds and im...
The CMC fluid mechanics program system was developed to transmit the theoretical solution of finite ...
A comprehensive aerodynamic analysis program based on linearized potential theory is described. The ...
This report documents the user input and output data requirements for the FEMNAS finite element Navi...
This report documents the user input and output data requirements for the FEMNAS finite element Navi...
An integrated system of computer programs for supersonic configurations is described. An explanation...
Through numerous summary examples, the scope and general nature of the computational fluid dynamics ...
A two dimensional unsteady Navier-Stokes calculation procedure with specific application to the isol...
The use of a computer code for the calculation of two dimensional inlet flow fields in a supersonic ...
Incompressible potential flow calculations are presented that were corrected for compressibility in ...
A weak interaction solution algorithm was established for aerodynamic flow about an isolated airfoil...
An integrated system of computer programs was developed for the design and analysis of supersonic co...
Computer programs to calculate the incompressible potential flow, corrected for compressibility, in ...
An order-of-magnitude analysis of the subsonic three dimensional steady time averaged Navier-Stokes ...
Papers given at the conference present the results of theoretical research on aerodynamic flow probl...
An aerodynamic analysis system based on potential theory at subsonic and/or supersonic speeds and im...
The CMC fluid mechanics program system was developed to transmit the theoretical solution of finite ...
A comprehensive aerodynamic analysis program based on linearized potential theory is described. The ...
This report documents the user input and output data requirements for the FEMNAS finite element Navi...
This report documents the user input and output data requirements for the FEMNAS finite element Navi...
An integrated system of computer programs for supersonic configurations is described. An explanation...
Through numerous summary examples, the scope and general nature of the computational fluid dynamics ...
A two dimensional unsteady Navier-Stokes calculation procedure with specific application to the isol...
The use of a computer code for the calculation of two dimensional inlet flow fields in a supersonic ...
Incompressible potential flow calculations are presented that were corrected for compressibility in ...