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Journals / International Journal of Aviation Science and Technology / 2022 / Volume: 03 Issue: 02

Numerical Analysis of Variable Morphing Wing for Improved Aerodynamic Performance of a Predator MQ-1B

Erdogan Kaygan(GIRNE AMERICAN UNIVERSITY)0000-0003-3319-3657
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Publication Date
2022-12-29
DOI
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AI Summary & Key Takeaways

AI Insight
⚡ TL;DR(Too Long; Didn't Read)

The results obtained from this work show that if morphing wings adapted to the Predator MQ-1B, it will provide significant performance benefits and also offer a great opportunity to reduce fuel consumption.

📌 3 Key Takeaways

🎯
Objective & Hypothesis:In this paper, aerodynamic performance benefits of morphing unmanned aerial vehicle’s wing concepts are investigated.
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Key Findings & Data:A Predator MQ-1B with variable wing structure was utilized for this study.
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Conclusion & Impact:The results obtained from this work show that if morphing wings adapted to the Predator MQ-1B, it will provide significant performance benefits and also offer a great opportunity to reduce fuel consumption.
🔬Design:Modeling & Simulation
📍Scope:Comprehensive Sample
⚙️Variables:Aerodynamics · morphing · predator

Abstract

In this paper, aerodynamic performance benefits of morphing unmanned aerial vehicle’s wing concepts are investigated. A Predator MQ-1B with variable wing structure was utilized for this study. The concept consists of variable twist (-10°< θ <10°, in steps of ±2.5°) and wing sweep (0°< θ <30°, in steps of +10°) to illustrate morphing wing’s performance benefits. All computations were performed with Athena Vortex Lattice modelling with varying degrees of twist and sweep angle considered. The results obtained from this work show that if morphing wings adapted to the Predator MQ-1B, it will provide significant performance benefits and also offer a great opportunity to reduce fuel consumption.

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Cite This Article

Kaygan, E. (2022). Numerical Analysis of Variable Morphing Wing for Improved Aerodynamic Performance of a Predator MQ-1B. International Journal of Aviation Science and Technology, Volume: 03 Issue: 02. https://ajindex.com/articles/1493707

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