阻力
Lift(数据挖掘)
控制理论(社会学)
风洞
模块化设计
工作(物理)
后掠翼
配置设计
升阻比
升力诱导阻力
机械
计算机科学
空气动力学
物理
控制(管理)
工程类
机械工程
数据挖掘
人工智能
操作系统
作者
Ronald C. Cheung,Djamel Rezgui,Jonathan E. Cooper,Richard Green,Raul C. Llamas-Sandin
摘要
View Video Presentation: https://doi.org/10.2514/6.2023-2458.vid In a V-tail configuration, the number of tail surfaces is reduced compared to the conventional configuration of horizontal and vertical stabilizers. Such configuration could benefit from lower weight and reduced drag if the overall wetted area is not required to increase to retain the same control and stability. Recent studies have considered forward-swept horizontal stabilizers for improving their achievable lift-curve slope through aeroelastic effects, with the aim of reducing the size and weight of the stabilizers without a loss of performance. Considering these potentially complementary attributes, this work explores combining these design concepts for improving the overall tail efficiency. A modular wind tunnel model is constructed and tested in a conventional empennage, a forward-swept V-tail and a backward-swept V-tail configuration to experimentally demonstrate the performance achieved. For this particular investigation, attention will be given to the lateral stability and control authority of the studied configurations.
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