High-Fidelity Computational Aerodynamics of the Elytron 4S …
https://ntrs.nasa.gov/api/citations/20180001906/downloads/20180001906.pdf
INTRODUCTIONNUMERICAL APPROACHOverset Grid GenerationHybrid turbulence modelingCase I, the glider The OVERFLOW code has a choice of algebraic, one-equation, and two-equation turbulence models (Ref. 4), including hybrid Reynolds-Averaged Navier-Stokes/Large Eddy Simulation (RANS/LES) models that close the RANS equations. In this study for the Elytron 4S UAV, the one equation Spalart-Allmaras (Ref. 10) turbulence model is used primarily within th... Author: Patricia Ventura Diaz, Seokkwan Yoon, Colin R. Theodore Publish Year: 2018
The OVERFLOW code has a choice of algebraic, one-equation, and two-equation turbulence models (Ref. 4), including hybrid Reynolds-Averaged Navier-Stokes/Large Eddy Simulation (RANS/LES) models that close the RANS equations. In this study for the Elytron 4S UAV, the one equation Spalart-Allmaras (Ref. 10) turbulence model is used primarily within th...
Author: Patricia Ventura Diaz, Seokkwan Yoon, Colin R. Theodore
Publish Year: 2018
DA: 96 PA: 98 MOZ Rank: 70