Transonic Aerodynamic Performance Analysis of a CRM Joined-Wing Configuration
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). The CRM wing, optimised for transonic flight, was t...
محفوظ في:
| المؤلفون الرئيسيون: | , , |
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| التنسيق: | Artigo |
| اللغة: | Inglês |
| منشور في: |
MDPI AG
2025-01-01
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| سلاسل: | Fluids |
| الموضوعات: | |
| الوصول للمادة أونلاين: | https://www.mdpi.com/2311-5521/10/2/27 |
| الوسوم: |
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