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迈向“超音速客机”新时代
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作者 黄建国 《海陆空天惯性世界》 2001年第1期18-20,共3页
2000年7月25日,一架载有100名旅客的"协和"飞机刚从世界著名的戴高乐机场起飞,2分钟后,就遭遇不策,飞机机翼着火,发动机爆炸。顺刻,飞机撞向巴黎北郊一座小旅馆上,酿成了机上9名机组人员共109人以及地面5人的悲惨事件。
关键词 超音速客机 “协和”客机 技术参数 飞行速度 摩擦高温 气动力中心 21世纪 层流控制技术
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Drag reduction via turbulent boundary layer flow control 被引量:11
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作者 ABBAS Adel BUGEDA Gabriel +5 位作者 FERRER Esteban FU Song PERIAUX Jacques PONS-PRATS Jordi VALERO Eusebio ZHENG Yao 《Science China(Technological Sciences)》 SCIE EI CAS CSCD 2017年第9期1281-1290,共10页
Turbulent boundary layer control(TBLC) for skin-friction drag reduction is a relatively new technology made possible through the advances in computational-simulation capabilities,which have improved the understanding ... Turbulent boundary layer control(TBLC) for skin-friction drag reduction is a relatively new technology made possible through the advances in computational-simulation capabilities,which have improved the understanding of the flow structures of turbulence.Advances in micro-electronic technology have enabled the fabrication of active device systems able to manipulating these structures.The combination of simulation,understanding and micro-actuation technologies offers new opportunities to significantly decrease drag,and by doing so,to increase fuel efficiency of future aircraft.The literature review that follows shows that the application of active control turbulent skin-friction drag reduction is considered of prime importance by industry,even though it is still at a low technology readiness level(TRL).This review presents the state of the art of different technologies oriented to the active and passive control for turbulent skin-friction drag reduction and contributes to the improvement of these technologies. 展开更多
关键词 turbulent boundary layer flow control drag reduction skin-friction drag reduction
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