Abstract
In the paper the turbulence models SA, SST and DES based on SA are compared for simulation of supersonic tip vortex at incoming flow Mach number M? = 3 and wing generator attack angles of 10 and 20 degrees. The simulations were carried out on the hybrid supercomputer system K-60 at the Keldysh Institute of Applied Mathematics RAS.
Full Text 
Sign-in/Register to access full text options
Sign-in/Register to access full text options 
Published version (
Free)
Free) 
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a call
