Outputs (3)

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.

Investigation of microjet engine inlet pressure distortions at angled inflow velocity conditions (2025)
Journal Article

The Armfield CM14 microjet axial flow turbine engine has been tested in open space at ambient conditions with engine inlet pressure at the aerodynamic interface plane (AIP) measured by a built-in pressure sensor for validating computational fluid dyn... Read More about Investigation of microjet engine inlet pressure distortions at angled inflow velocity conditions.

Transonic aerodynamic performance analysis of a CRM joined-wing configuration (2025)
Journal Article

This study examines the aerodynamic performance of a joined-wing (JW) aircraft design based on the NASA Common Research Model (CRM), aiming to assess its potential for efficient commercial transport or cargo aircraft at transonic speed (Mach 0.85). T... Read More about Transonic aerodynamic performance analysis of a CRM joined-wing configuration.