Recent progress in the study of transition in the hypersonic boundary layer

• 来源期刊: 国家科学评论（英文版）
• 关键词: hypersonic boundary layer transition quiet wind tunnel
• 年，卷（期）: 2019,（1）
• 页码范围: 155-170
• 页数: 16页
• 语种: 英文
• DOI: 10.1093/nsr/nwy052

摘要

Turbulence is a universal form of fluid motion.It is the key issue in fluid mechanics.Very recently,it has become a bottleneck in some key engineering research of national importance,such as aeronautics,astronautics and navigation.Developed turbulence and the onset of turbulence,i.e.transition,are two interrelated parts of turbulence.T-he hypersonic boundary-layer transition is a strategic focus in the fluid mechanics community.T-his article reviews recent developments in the study of the hypersonic boundary-layer transition,research facilities and experimental techniques.The hypersonic quiet wind tunnel is introduced as a necessary device to obtain real flight data in near space.Near-wall measurement techniques,such as temperature-sensitive paint,near-wall particle image velocimetry and Rayleigh-scattering visualization,are shown.The most important issues in the recent development of the transition in the hypersonic boundary layer are addressed.The instability and nonlinear interaction of different instability modes are discussed.The recent contributions from China,especially at Peking University,are also introduced.