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Aerodynamic and Structural Design Procedures Supported by Fabrication and Flight Testing of a Small Unmanned Helicopter

Amr Mansour Mohammed Kassem A.M.Abdel-Rahman Mohamed Y.Zakaria

无人系统(英文)2025,Vol.13Issue(3):709-736,28.
无人系统(英文)2025,Vol.13Issue(3):709-736,28.DOI:10.1142/S230138502550044X

Aerodynamic and Structural Design Procedures Supported by Fabrication and Flight Testing of a Small Unmanned Helicopter

Aerodynamic and Structural Design Procedures Supported by Fabrication and Flight Testing of a Small Unmanned Helicopter

Amr Mansour 1Mohammed Kassem 1A.M.Abdel-Rahman 1Mohamed Y.Zakaria1

作者信息

  • 1. Military Technical College,Kobry El-Kobbah,Cairo 11766,Egypt
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摘要

关键词

Rotary blade/CFD/VTOL/unmanned helicopter/blade design/composite

Key words

Rotary blade/CFD/VTOL/unmanned helicopter/blade design/composite

引用本文复制引用

Amr Mansour,Mohammed Kassem,A.M.Abdel-Rahman,Mohamed Y.Zakaria..Aerodynamic and Structural Design Procedures Supported by Fabrication and Flight Testing of a Small Unmanned Helicopter[J].无人系统(英文),2025,13(3):709-736,28.

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