原文传递
The conceptual design of a Mach 2 Oblique Flying Wing supersonic transport
| 题名： | The conceptual design of a Mach 2 Oblique Flying Wing supersonic transport |
| 作者： | Vandervelden, Alexander J. M. |
| 关键词： | supersonic；transport；design；concept；mach；ying；stability；technology；balance；dynamics |
| 摘要： | This paper is based on a performance and economics study of a Mach two oblique flying wing transport aircraft that is to replace the B747B. In order to fairly compare our configuration with the B747B an equal structural technology level is assumed. It will be shown that the oblique flying wing configuration will equal or outperform the B747 in speed, economy and comfort while a modern stability and control system will balance the aircraft and smooth out gusts. The aircraft is designed to comply with the FAR25 airworthiness requirements and FAR36 stage 3 noise regulations. Geometry, aerodynamics, stability and control parameters of the oblique flying wing transport are discussed. |
| 报告类型： | 科技报告 |
相关文献
- Large capacity oblique all-wing transport aircraft
- Development of Doppler Global Velocimetry as a Flow Diagnostics Tool
- Enabling Rapid and Robust Structural Analysis During Conceptual Design.
- Shape Sensing for Wings with Spars and Ribs Using Simulated Strain.
- The 1990 high-speed civil transport studies
- Automation of Structural Sizing of Aircraft Concepts Under Static Aeroelastic Constraints [STUB].
检索历史
应用推荐
