| 标题 |
 Mission-Specific Preliminary Design and Weight Optimization for High-Speed Vertical Takeoff and Landing (HSVTOL) Aircraft 高速垂直起降（HSVTOL）飞机特定任务初步设计和重量优化
相关领域
起飞
起飞和着陆
航空航天工程
航空学
汽车工程
工程类
计算机科学
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| 网址 | |
| DOI | |
| 其它 | This paper leverages public domain information to reevaluate existing technology and explore the potential for advancements in High-Speed Vertical Takeoff and Landing (HSVTOL) aircraft design. Focusing on preliminary design, analysis, and technological innovations, the study aims to identify opportunities for improvement and tailor the proposed HSVTOL aircraft to address specific mission requirements. Key design elements include a balance between wing loading and disk loading as the main parameters. Through mission analysis, design optimizations, and the evaluation of potential technological enhancements, the findings contribute to advancing VTOL aircraft design. The research highlights potential innovations and improvements that can be applied to future HSVTOL platforms, expanding the capabilities of high-speed vertical takeoff and landing operations. |
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