Add to ORKGThesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1989.Includes bibliographical references (v.2, leaves 174-187).by Bernard Loyd.Ph.D
An upwind MUSCL type implicit scheme for the three-dimensional Navier-Stokes equations is presented....
The conservative unsteady Euler equations for the flow relative motion in the moving frame of refere...
The field of Computational Fluid Dynamics (CFD) is in a continual state of advancement due to new nu...
A novel semi-implicit scheme for the Navier-Stokes equations is presented and evaluated. The semi-i...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1990.Ti...
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1993....
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1989.In...
The feasibility was determined of incorporating the Navier-Stokes computational code, CFL3D, into th...
This project is a continuation of the work performed in the summers of 1991 and 1992, during which a...
Steady solutions about a slender sharp edged delta wing in a supersonic freestream for moderate and ...
Five viscous transonic airfoil cases were computed by two significantly different computational flui...
An embedded grid algorithm for the Euler and/or Navier-Stokes equations is developed and applied to ...
A solution method for the three-dimensional Euler equations is formulated and implemented. The solv...
Models of four delta wings were built and tested in the 8 x 8 ft Transonic Wind Tunnel at LaRC. The ...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1996.In...
An upwind MUSCL type implicit scheme for the three-dimensional Navier-Stokes equations is presented....
The conservative unsteady Euler equations for the flow relative motion in the moving frame of refere...
The field of Computational Fluid Dynamics (CFD) is in a continual state of advancement due to new nu...
A novel semi-implicit scheme for the Navier-Stokes equations is presented and evaluated. The semi-i...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1990.Ti...
Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1993....
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1989.In...
The feasibility was determined of incorporating the Navier-Stokes computational code, CFL3D, into th...
This project is a continuation of the work performed in the summers of 1991 and 1992, during which a...
Steady solutions about a slender sharp edged delta wing in a supersonic freestream for moderate and ...
Five viscous transonic airfoil cases were computed by two significantly different computational flui...
An embedded grid algorithm for the Euler and/or Navier-Stokes equations is developed and applied to ...
A solution method for the three-dimensional Euler equations is formulated and implemented. The solv...
Models of four delta wings were built and tested in the 8 x 8 ft Transonic Wind Tunnel at LaRC. The ...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1996.In...
An upwind MUSCL type implicit scheme for the three-dimensional Navier-Stokes equations is presented....
The conservative unsteady Euler equations for the flow relative motion in the moving frame of refere...
The field of Computational Fluid Dynamics (CFD) is in a continual state of advancement due to new nu...