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matteobernardini / STREAmS

Supersonic TuRbulEnt Accelerated navier stokes Solver
GNU General Public License v3.0
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Field files and Shock Impingement location (Shock wave Boundary layer Interaction case) #4

Closed Sushmitha46 closed 2 years ago

Sushmitha46 commented 2 years ago

Hello,

  1. I wanted to know at what intervals are field files getting generated, if I want them to be written for every 10,000 iterations is it possible to do so? or is there any other logic behind how these files are being written?
  2. If I wanted to run the SBLI case for different Mach Numbers or for different shock deflection Angles will I have to change the variable "xshock_imp"?

Thank you.

davidem88 commented 2 years ago

1) 3D fields are written at constant time intervals. The variable "dtsave" in input.dat is the time interval at which 3D solutions are written 2) The variable "Mach" in input.dat is the free-stream Mach number. xshock_imp is the nominal impingement location of the inviscid shock, and "deflec_shock" is the shock angle. These three parameters are independent. Of course you have to make sure that they fall into the computational domain and that xshock_imp is after the recycling station.

Sushmitha46 commented 2 years ago

Thank you for the clarification.