Experimental Investigations of a Generic Swept Unmanned Combat Air Vehicle with Controls

Vicroy Dan D.; Huber Kerstin C.; Schuette Andreas; Rein Martin; Irving Jonathan P.; Rigby Glyn; Loeser Thomas; Huebner Andreas-Rene; Birch Trevor J.

首页> 外文期刊>Journal of Aircraft >Experimental Investigations of a Generic Swept Unmanned Combat Air Vehicle with Controls

【24h】

Experimental Investigations of a Generic Swept Unmanned Combat Air Vehicle with Controls

机译：通用扫频无人战斗机控制实验研究

获取原文

获取原文并翻译 | 示例

掌桥外文数据库（机构版） >>

开具论文收录证明 >>

文献代查 >>

页面导航

摘要
著录项
相似文献
相关主题

摘要

Several static and dynamic forced-motion wind-tunnel tests on a generic unmanned combat air vehicle configuration with a 53 deg swept leading edge are reviewed. The static tests include both subsonic and transonic measurements. These tests are part of an international research effort to assess and advance the state-of-the-art of computational-fluid-dynamics methods to predict the static and dynamic stability and control characteristics for this type of configuration. The tests included analysis of trailing-edge control surface effectiveness. This paper describes the data collected from three different models of this unmanned combat air vehicle configuration in four different wind tunnels. A subset of this large experimental dataset was selected as focus test cases for computational-fluid-dynamics comparison. The focus test case data are presented in detail.

机译：回顾了对具有53度前掠角的通用无人驾驶飞行器配置的几种静态和动态强制运动风洞测试。静态测试包括亚音速和跨音速测量。这些测试是一项国际研究工作的一部分，该工作旨在评估和推进最新的计算流体动力学方法，以预测此类配置的静态和动态稳定性以及控制特性。测试包括对后缘控制面有效性的分析。本文描述了从四种不同风洞中的这种无人作战飞机配置的三种不同模型收集的数据。选择了这个大型实验数据集的一个子集作为重点测试用例，以进行计算流体动力学比较。重点测试案例数据将详细介绍。

著录项

来源
《Journal of Aircraft》 |2018年第2期|475-501|共27页
作者
Vicroy Dan D.; Huber Kerstin C.; Schuette Andreas; Rein Martin; Irving Jonathan P.; Rigby Glyn; Loeser Thomas; Huebner Andreas-Rene; Birch Trevor J.;
展开▼
作者单位

NASA Langley Res Ctr, Flight Dynam Branch, Res Directorate, MS 308, Hampton, VA 23681 USA;

German Aerosp Ctr, DLR, Inst Aerodynam & Flow Technol, Lilienthalpl 7, D-38108 Braunschweig, Germany;

German Aerosp Ctr, DLR, Inst Aerodynam & Flow Technol, Lilienthalpl 7, D-38108 Braunschweig, Germany;

German Aerosp Ctr, DLR, Inst Aerodynam & Flow Technol, Bunsenstr 10, D-37073 Gottingen, Germany;

BAE Syst Mil Air & Informat, Warton PR4 1AX, England;

BAE Syst Mil Air & Informat, Warton PR4 1AX, England;

German Dutch Wind Tunnels, DNW, Low Speed Wind Tunnel, Lilienthalpl 7, D-38108 Braunschweig, Germany;

German Dutch Wind Tunnels, DNW, Low Speed Wind Tunnel, Lilienthalpl 7, D-38108 Braunschweig, Germany;

Def Sci & Technol Lab, Aerosp Sci, Portsdown Hill Rd, Fareham PO17 6AD, England;

展开▼
收录信息美国《科学引文索引》(SCI);美国《工程索引》(EI);
原文格式 PDF
正文语种 eng
中图分类
关键词

相似文献

外文文献
中文文献
专利

1. Integrated Computational/Experimental Approach to Unmanned Combat Air Vehicle Stability and Control Estimation [J] . Russell M. Cummings, Andreas Schuette Journal of Aircraft . 2012,第6期

机译：无人战斗机稳定性和控制估计的综合计算/实验方法
2. Static and Forced-Oscillation Tests of a Generic Unmanned Combat Air Vehicle [J] . Dan D. Vicroy, Thomas D. Loeser, Andreas Schuette Journal of Aircraft . 2012,第6期

机译：通用无人驾驶飞行器的静态和强迫振荡测试
3. Prediction of Control Effectiveness for a Highly Swept Unmanned Air Vehicle Configuration [J] . Coppin Joe, Birch Trevor, Kennett David, Journal of Aircraft . 2018,第2期

机译：高扫频无人机配置控制效果的预测
4. Naval Air Systems Command (NAVAIR) Unmanned Aerial Vehicle (UAV) Unmanned Combat Aerial Vehicle (UCAV) Distributed Simulation Infrastructure [C] . American Institute of Aeronautics and Astronautics "Unmanned Unlimited" Systems, Technologies, and Operations — Aerospace, Land, and Sea Conference and Workshop Exhibit . 2003

机译：Naval Air Systems命令（Navair）无人驾驶车辆（UAV）无人战斗机（UCAV）分布式仿真基础设施
5. Aerodynamics of unmanned combat air vehicles: Flow structure and control. [D] . Elkhoury, Michel. 2004

机译：无人作战飞机的空气动力学：流动结构和控制。
6. Mobility Control of Unmanned Aerial Vehicle as Communication Relay to Optimize Ground-to-Air Uplinks [O] . Gaofeng Wu, Xiaoguang Gao, Kaifang Wan 2020

机译：无人飞行器作为通信中继的移动性控制以优化地对空上行链路
7. Autonomous Control of Combat Unmanned Aerial Vehicles to Evade Surface-to-Air Missiles Using Deep Reinforcement Learning [O] . Gyeong Taek Lee, Chang Ouk Kim 2020

机译：作者：王莹，王莹，王莹，王莹，王建华
8. Origin and Control of the Flow Structure on Unmanned Combat Air Vehicle [R] . Rockwell, D. , Yaniktepe, B. , Yavuz, M. M. , 2007

机译：无人作战飞行器流动结构的起源与控制

Experimental Investigations of a Generic Swept Unmanned Combat Air Vehicle with Controls

摘要

著录项

相似文献

相关主题

期刊订阅