Open AccessA comparative study of URANS, DDES and DES simulations of Jetstream 31 aircraft near the compressibility limit
Author(s) -
Hrishabh Chaudhary,
Nicolas Ledos,
László Könözsy
Publication year - 2021
Publication title -
journal of computational and applied mechanics
Language(s) - English
Resource type - Journals
eISSN - 2732-0189
pISSN - 1586-2070
DOI - 10.32973/jcam.2021.009
Subject(s) - detached eddy simulation , turbulence , turbulence modeling , computational fluid dynamics , wind tunnel , lift coefficient , aerodynamics , lift (data mining) , drag coefficient , mechanics , drag , reynolds averaged navier–stokes equations , physics , aerospace engineering , reynolds number , engineering , computer science , data mining
This work presents a comparative study of Unsteady Reynolds–Averaged Navier–Stokes (URANS), Detached Eddy Simulations (DES) and Delayed Detached Eddy Simulations (DDES) turbulence modeling approaches by performing numerical investigation with the ANSYS-FLUENT software package on a full-scale model of the Jetstream 31 aircraft. The lift and drag coefficients obtained from different models are compared with flight test data, wind tunnel data and theoretical estimates. The different turbulence models are also compared with each other on the basis of pressure coefficient distributions and velocity fluctuations along various lines and sections of the aircraft. For the mesh and the conditions presented in this study, the DDES Spalart–Allmaras model gives the best overall results.