Presentations given at the NASA Computational Fluid Dynamics (CFD) Conference held at the NASA Ames Research Center, Moffett Field, California, March 7-9, 1989 are given. Topics covered include research facility overviews of CFD research and applications, validation programs, direct simulation of compressible turbulence, turbulence modeling, advances in Runge-Kutta schemes for solving 3-D Navier-Stokes equations, grid generation and invicid flow computation around aircraft geometries, numerical simulation of rotorcraft, and viscous drag prediction for rotor blades
A computer code called Proteus 2D was developed to solve the two-dimensional planar or axisymmetric,...
The F/A-18A aircraft has experienced engine stalls at high angles-of-attack and yaw flight condition...
A multidisciplinary, finite element-based, highly graphics-oriented, linear and nonlinear analysis c...
The work completed to date is comprised of the following: a simple vehicle model representative of t...
This Workshop on Stratospheric Models and Measurements (M&M) marks a significant expansion in the hi...
This Workshop on Stratospheric Models and Measurements (M&M) marks a significant expansion in the hi...
The purpose of this research is to establish a computational model of the dynamics in a fluidic osci...
The development and applications of multiblock/multizone and adaptive grid methodologies for solving...
Advanced high performance vehicles, including Single-Stage-To-Orbit (SSTO) hypersonic flight vehicle...
A general purpose, three-dimensional computational fluid dynamics code named PHOENICS, developed by ...
The research and technology accomplishments of the NASA Lewis Research Center are summarized for the...
An advanced engineering model has been developed to aid in the analysis and design of hydrogen/oxyge...
This report provides the analytical documentation for the SOURCE3D Rotor Wake/Stator Interaction Cod...
A new computer code was developed to solve the two-dimensional or axisymmetric, Reynolds averaged, u...
A successful design of a space-based or ground optical system requires an iterative procedure which ...
A computer code called Proteus 2D was developed to solve the two-dimensional planar or axisymmetric,...
The F/A-18A aircraft has experienced engine stalls at high angles-of-attack and yaw flight condition...
A multidisciplinary, finite element-based, highly graphics-oriented, linear and nonlinear analysis c...
The work completed to date is comprised of the following: a simple vehicle model representative of t...
This Workshop on Stratospheric Models and Measurements (M&M) marks a significant expansion in the hi...
This Workshop on Stratospheric Models and Measurements (M&M) marks a significant expansion in the hi...
The purpose of this research is to establish a computational model of the dynamics in a fluidic osci...
The development and applications of multiblock/multizone and adaptive grid methodologies for solving...
Advanced high performance vehicles, including Single-Stage-To-Orbit (SSTO) hypersonic flight vehicle...
A general purpose, three-dimensional computational fluid dynamics code named PHOENICS, developed by ...
The research and technology accomplishments of the NASA Lewis Research Center are summarized for the...
An advanced engineering model has been developed to aid in the analysis and design of hydrogen/oxyge...
This report provides the analytical documentation for the SOURCE3D Rotor Wake/Stator Interaction Cod...
A new computer code was developed to solve the two-dimensional or axisymmetric, Reynolds averaged, u...
A successful design of a space-based or ground optical system requires an iterative procedure which ...
A computer code called Proteus 2D was developed to solve the two-dimensional planar or axisymmetric,...
The F/A-18A aircraft has experienced engine stalls at high angles-of-attack and yaw flight condition...
A multidisciplinary, finite element-based, highly graphics-oriented, linear and nonlinear analysis c...