Abstract
A numerical method for solving the Reynolds-averaged Navier-Stokes equations around axisymmetric afterbody/nozzle configurations, with sharp trailing edges or finite bases, is presented. Turbulence closure is achieved through either a simple algebraic turbulence model or a low Reynolds number form of the A>e two-equation differential model. The solution procedure uses an explicit time-marching finite-volume method. The performance of each of the turbulence models is assessed through comparisons with experimental data on three series of geometries, including both attached and separated flow cases.
Sign-in/Register to access full text options 
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 callDisclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.
