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Conceptual Design and Integrated Parametric Framework for Aerodynamic Optimization of Morphing Subsonic Blended-Wing-Body UAVs

This paper presents a unified aerodynamic design and optimization framework for morphing Blended-Wing-Body (BWB) Unmanned Aerial Vehicles (UAVs) operating in subsonic and near-transonic regimes. The proposed framework integrates parametric CAD modeling, Computational Fluid Dynamics (CFD), and surrog...

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Asıl Yazarlar: Liguang Kang, Sandeep Suresh Babu, Muhammet Muaz Yalçın, Abdel-Hamid Ismail Mourad, Mostafa S. A. ElSayed
Materyal Türü: Artigo
Dil:Inglês
Baskı/Yayın Bilgisi: MDPI AG 2026-01-01
Seri Bilgileri:Applied Mechanics
Konular:
UAV
blended wing body
aerodynamic optimization
response surface methodology
subsonic aerodynamics
CFD
Online Erişim:https://www.mdpi.com/2673-3161/7/1/5
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