混合翼身飞机在平静/波浪水面上的跳水运动数值研究

IF 1.5 3区 工程技术 Q2 ENGINEERING, AEROSPACE Journal of Aircraft Pub Date : 2024-09-12 DOI:10.2514/1.c037721
Shili Ding, Peiqing Liu, Xueliang Wen, Qiulin Qu
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Numerical Study of Skipping Motion of Blended-Wing–Body Aircraft Ditching on Calm/Wavy Water
Journal of Aircraft, Ahead of Print.
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来源期刊
Journal of Aircraft
Journal of Aircraft 工程技术-工程:宇航
CiteScore
4.50
自引率
31.80%
发文量
141
审稿时长
6 months
期刊介绍: This Journal is devoted to the advancement of the applied science and technology of airborne flight through the dissemination of original archival papers describing significant advances in aircraft, the operation of aircraft, and applications of aircraft technology to other fields. The Journal publishes qualified papers on aircraft systems, air transportation, air traffic management, and multidisciplinary design optimization of aircraft, flight mechanics, flight and ground testing, applied computational fluid dynamics, flight safety, weather and noise hazards, human factors, airport design, airline operations, application of computers to aircraft including artificial intelligence/expert systems, production methods, engineering economic analyses, affordability, reliability, maintainability, and logistics support, integration of propulsion and control systems into aircraft design and operations, aircraft aerodynamics (including unsteady aerodynamics), structural design/dynamics , aeroelasticity, and aeroacoustics. It publishes papers on general aviation, military and civilian aircraft, UAV, STOL and V/STOL, subsonic, supersonic, transonic, and hypersonic aircraft. Papers are sought which comprehensively survey results of recent technical work with emphasis on aircraft technology application.
期刊最新文献
Experimental Study on a Liquid Hydrogen Tank for Unmanned Aerial Vehicle Applications Numerical Study of Skipping Motion of Blended-Wing–Body Aircraft Ditching on Calm/Wavy Water Blended-Wing-Body Regional Aircraft Optimization with High-Fidelity Aerodynamics and Critical Design Requirements Towards Wall-Resolved Large-Eddy Simulation of the High-Lift Common Research Model Investigation of Hybrid Laminar Flow Control Capabilities from the Flight Envelope Perspective
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