sm_data
收藏资源简介：
| FILENAME | TASKTYPE | TASK | SAMPLES | PARAMINPUT | GEOMINPUT | OUTPUT | |----------|----------|------|----------|------------|-----------|--------| |shocktube.h5 | 二维瞬态 | 二维激波管问题 | 1500 | NAN | (1500,16384,6)=x+y+初始密度+压强+vx+vy | (1500,16384,21,4)=密度+压强+vx+vy | | burgers_invis.h5 | 二维瞬态 | Burgers方程 | 1100 | NAN | (1100,128,128,3)=x+y+初始 | (1000,128,128,50,1) | | naca.h5 | 二维稳态 | 机翼二维空气动力模拟 | 2490 | (2490,9) | (2490,4025,2) | (2490,4025,5) | | darcy_1.h5 | 二维稳态 | DarcyFlow | 10000 | NAN | (10000,128,128,3)=x+y+粘性 | (10000,128,128,1) | | turbulence.h5 | 二维稳态 | 湍流 | 400 | NAN | (400, 2673, 3)=x+y+? | (400, 2673, 1)=? | | liddrivencavity.h5 | 二维稳态 | 绕流+方腔驱动流 | 1000 | (1000,2)=Reynolds+Grashof | (1000,128,128,4)=x+y+障碍物几何掩码+障碍物SDF | (1000,128,128,4)=vx+vy+压强+温度 | | bloodflow.h5 | 三维瞬态 | 血液动力学模拟 | 500 | (500,121,6) | (1656,3) | (500,1656,121,3)=vx+vy+vz | | dtchull.h5 | 三维稳态 | 轮船水动力模拟 | 137 | 137*(1)=Angle | 137*(229343~247394,3) | 137*(229343~247394,4) | | nasacrm.h5 | 三维稳态 | 飞机三维空气动力模拟 | 44 | (44,6) | (44,454404,3) | (44,454404,4)=cp+cfx+cfy+cfz | | aircraft.h5 | 三维稳态 | 飞机三维空气动力模拟 | 150 | (150,4)=Machx+Machy+Machz+Geomid | (150,331971,3) | (150,331971,6)=cp+rho+u+v+w+pressure | | carcrash.h5 | 三维稳态 | 汽车碰撞问题 | 131 | (131,2)=vx+vy | (1096119,3) | (131,1096119,1)=最大应力 |
