SimCafe

Space shortcuts

Child pages
  • Supersonic Flow Over a Wedge - Verification & Validation

Versions Compared

Old Version 41

changes.mady.by.user user-6c822

Saved on

compared with

New Version 42

changes.mady.by.user user-6c822

Saved on

Key

  • This line was added.
  • This line was removed.
  • Formatting was changed.

...


Mach Number

Static Pressure (atm)

Shock Angle (degrees)

Theory Value

2.254

2.824

32.22

FLUENT Solution

2.243

2.803

34.99

Percent Difference

0.8%

0.7%

8.2%

Continue to Exercises