A potentially gridless solution method for the compressible Euler/Navier-Stokes equations
類似資料:
National Aeronautics and Space Administration |
National Aeronautics and Space Adminstration |
American Institute of Aeronautics and Astronautics |
8
テクニカルペーパー
Navier-Stokes Simulations of a Supersonic Jet in Transonic Crossflow: Comparison to Surface Data.
American Institute of Aeronautics and Astronautics |
3
テクニカルペーパー
A STABLE PENALTY METHOD FOR THE COMPRESSIBLE NAVIER-STOKES EQUATION. I. OPEN BOUNDARY CONDITIONS
National Aeronautics and Space Adminstration |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
5
テクニカルペーパー
A Modified Space-Time Conservation Element and Solution Element Method for Euler and Navier Stokes Equations
American Institute of Aeronautics and Astronautics |
11
テクニカルペーパー
Cartesian Grid Solution of the Euler Equations Using a Gridless Boundary Condition Treatment
American Institute of Aeronautics and Astronautics |
National Aeronautics and Space Adminstration |
American Institute of Aeronautics and Astronautics |