skip to content

Public Access (formerly Langley Research Center)

Turbulence Modeling Resource


 

 

Return to: Axisymmetric Near-Sonic Jet Case Intro Page

Return to: Turbulence Modeling Resource Home Page


 

Axisymmetric Near-Sonic Jet Validation Case

Effect of Reference Mach Number
 

SA - effect of reference Mach number on u along y=0 SST-Vm - effect of reference Mach number on u along y=0

The plots show examples of the effect of different values of freestream Mach number on the computed centerline velocity (on the 49x49; 31x49; 129x113 grid). Note that the reference Reynolds number is also affected proportionally. Some CFD codes have difficulty computing with quiescent outer conditions, so Mref=0.01 (red curve) is recommended as a reasonable compromise.
 
 

Return to: Axisymmetric Near-Sonic Jet Case Intro Page

Return to: Turbulence Modeling Resource Home Page


 
 



Page Curators: Christopher Rumsey, Ethan Vogel, Clark Pederson
Last Updated: 08/28/2020