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...

पूर्ण विवरण

ग्रंथसूची विवरण

मुख्य लेखकों:	Liguang Kang, Sandeep Suresh Babu, Muhammet Muaz Yalçın, Abdel-Hamid Ismail Mourad, Mostafa S. A. ElSayed
स्वरूप:	Artigo
भाषा:	Inglês
प्रकाशित:	MDPI AG 2026-01-01
श्रृंखला:	Applied Mechanics
विषय:	UAV blended wing body aerodynamic optimization response surface methodology subsonic aerodynamics CFD
ऑनलाइन पहुंच:	https://www.mdpi.com/2673-3161/7/1/5
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