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.