Prandtl Meyer Shock problem

1.Shock Flow Boundaries:

For solvind steadystate flow appropriate boundary conditions are neededthat is mathematical model.For solving transient flow appropriate initila conditions are needed.there are three types of boudary conditions Drichilet,Neuman,and mixed boundary conditions.

2.Shock Wave:

When a speed of the moving object or source exceeds the sound of the medium then the wavefront lag behind the source forming the cone shaped source at vertex,the edge of the cone forms supersonic wavefront with a unusual large amplitude called shock wave.

3.Effect Of SGS Parameters :

Temperature Animation For SGS 0.05k

Pressur Animation For SGS 0.05k

Pressure Animation For SGS 0.1k

Temperature Animation For 0.1k

Pressure Animation For SGS 0.01k

Temperature Animation For 0.01k