SFB 255: Transatmospheric Flight Systems - Fundamentals of Aerothermodynamics, Powerplants and Flight Mechanics

SFB 255：跨大气层飞行系统 - 空气热力学、动力装置和飞行力学基础

• 批准号: 5475209
• 金额: --
• 依托单位: Technische Universität München (TUM)
• 依托单位国家: 德国
• 项目类别: Collaborative Research Centres
• 财政年份: 1989
• 资助国家: 德国
• 起止时间: 1988-12-31 至 2002-12-31
• 项目状态: 已结题
• 来源: https://gepris.dfg.de/gepris/projekt/5475209?language=en
• 关键词: SFB; 255; Transatmospheric; Flight; Systems

The collaborative research centre 255 is concerned with research of hypersonic flight fundamentals. The great challenges of hypersonic flight are due to basic technical-scientific problems in several areas to which aerothermodynamics, propulsion and flight mechanics belong. A central issue is the capability for a flight at very high speed using aerodynamic lift and air-breathing propulsion, with extreme performance requirements to be met in regard to payload or range, respectively. The inherent, high complexity of such flight systems requires a close, interdisciplinary cooperation.

255合作研究中心关注高超音速飞行基础的研究。高超声速飞行的巨大挑战是由于空气热力学、推进和飞行力学属于几个领域的基本技术科学问题。一个核心问题是使用空气动力升力和吸气推进的高速飞行能力，分别在有效载荷或航程方面满足极端性能要求。这种飞行系统固有的高度复杂性需要密切的跨学科合作。