Improved Delayed Detached Eddy Simulations Applied to a NACA0015 Aerofoil Subject to Acoustic Excitation (2022)

First Author: Coskun S
Attributed to:  Flow Control through Acoustic Excitation to Improve Future Aero-engine Performance funded by EPSRC

Abstract

No abstract provided

Bibliographic Information

Digital Object Identifier: http://dx.doi.org/10.2514/6.2022-3237

Publication URI: http://dx.doi.org/10.2514/6.2022-3237

Type: Conference/Paper/Proceeding/Abstract