· Mach 1.6
flow past a blunt-nose-cylinder projectile at 4o
angle of attack (NASA-TMX-3558).
· Mach 1.2
flow past an ellipse-cylinder projectile at 8o
angle of attack.
· Mach 1.4
flow past a 4% circular bump.
· Mach 1.4
flow past a sphere.
· Generating
3D finite element mesh for canard-wing-tail-body combination.
· Canard-wing-tail-body
combination meshes generation (1).
· Canard-wing-tail-body
combination meshes generation (2).
·
Mach 1.2 flow passes canard-wing-tail-body at 10o angle of attack.
·
Mach 1.2 flow past the
elliptical rocket at 10 degrees angle of attack.
· Mach 1.8 flow passes a 5o
cone at 45o angle of attack.
· Mach 7.4 flow past a 75o swept
ellipse cone at 15o angle of attack.
· Mach 1.76 shock wave out of a cylindrical
tube.
·
Flow discharges from a 25o or 45
o convergent nozzles with P/P¥=4.0.
·
Mach 0.94, 0.96 and 1.2 flow
past a secant-ogiv-cylinder-boattail projectile.
· Mach 1.2
flow past a NACA0012 airfoil at 0o
angle of attack
· Mach 1.2
flow past a NACA0012 airfoil at 7o
angle of attack
· Transient
Solution at 6.1 m Second for The Sod’s
Shock Tube.
· Reflection
of a Cylindrical Convergent Shock Wave.
· Helium
Exploded Into Surrounded Air.