Broadband and transient aeroacoustic analysis of a CRM-based joined wing configuration at low speeds
(2025)
Presentation / Conference Contribution
This study presents a computational investigation into the aeroacoustic performance of a Joined Wing (JW) configuration at low subsonic speeds. The modelled JW geometry, derived from NASA’s Common Research Model (CRM) configuration, consists of a fro... Read More about Broadband and transient aeroacoustic analysis of a CRM-based joined wing configuration at low speeds.