Add to ORKGThe development of the RPLUS2D/3D codes is summarized. These codes utilize LU algorithms to solve chemical non-equilibrium flows in a body-fitted coordinate system. The motivation behind the development of these codes is the need to numerically predict chemical non-equilibrium flows for the National AeroSpace Plane Program. Recent improvements include vectorization method, blocking algorithms for geometric flexibility, out-of-core storage for large-size problems, and an LU-SW/UP combination for CPU-time efficiency and solution quality
Major upgrades have been made in two of the programs reported in "ive Computer Codes for Analysis of...
A second order Alternating Direction Implicit/Explicit computer code, or SADIE for short, has been d...
The history of the Computational Fluids Laboratory -3D (CFL3D) Navier-Stokes computer code is discus...
To support the National Aerospace Plane project, the RPLUS3D CFD code has been developed at NASA Lew...
A 3-D numerical program that incorporates comprehensive real gas property models was developed to si...
An effort is currently underway at NASA Lewis to develop two- and three-dimensional Navier-Stokes co...
A numerical procedure was developed to compute the inviscid super/hypersonic flow field about comple...
Two new parabolized Navier-Stokes (PNS) codes were developed to compute the three-dimensional, visco...
The main objective of this research was to develop an efficient three-dimensional computer code for ...
Under this grant, two numerical algorithms were developed to predict the flow of viscous, hypersonic...
and three ' dimen-sions have been developed at NASA Ames and have been widely distributed since...
Presented is a collection of papers on research activities carried out during the funding period of ...
The problem of interest here is the analysis of chemically reacting flow inside of supersonic ramjet...
A new three-dimensional numerical program incorporated with comprehensive real gas property models w...
This final report summarizes the research accomplished. The research performed during the grant peri...
Major upgrades have been made in two of the programs reported in "ive Computer Codes for Analysis of...
A second order Alternating Direction Implicit/Explicit computer code, or SADIE for short, has been d...
The history of the Computational Fluids Laboratory -3D (CFL3D) Navier-Stokes computer code is discus...
To support the National Aerospace Plane project, the RPLUS3D CFD code has been developed at NASA Lew...
A 3-D numerical program that incorporates comprehensive real gas property models was developed to si...
An effort is currently underway at NASA Lewis to develop two- and three-dimensional Navier-Stokes co...
A numerical procedure was developed to compute the inviscid super/hypersonic flow field about comple...
Two new parabolized Navier-Stokes (PNS) codes were developed to compute the three-dimensional, visco...
The main objective of this research was to develop an efficient three-dimensional computer code for ...
Under this grant, two numerical algorithms were developed to predict the flow of viscous, hypersonic...
and three ' dimen-sions have been developed at NASA Ames and have been widely distributed since...
Presented is a collection of papers on research activities carried out during the funding period of ...
The problem of interest here is the analysis of chemically reacting flow inside of supersonic ramjet...
A new three-dimensional numerical program incorporated with comprehensive real gas property models w...
This final report summarizes the research accomplished. The research performed during the grant peri...
Major upgrades have been made in two of the programs reported in "ive Computer Codes for Analysis of...
A second order Alternating Direction Implicit/Explicit computer code, or SADIE for short, has been d...
The history of the Computational Fluids Laboratory -3D (CFL3D) Navier-Stokes computer code is discus...