Visualization of massive separation of unstarted inlet
暂无分享,去创建一个
[1] William H. Heiser,et al. Hypersonic Airbreathing Propulsion , 1994 .
[2] S. Im,et al. Visualizing supersonic inlet duct unstart using planar laser Rayleigh scattering , 2011 .
[3] Liu Weidong,et al. Experimental investigation of the micro-ramp based shock wave and turbulent boundary layer interaction control , 2012 .
[4] M. Samimy,et al. Streamwise structures in a turbulent supersonic boundary layer , 1994 .
[5] David Van Wie,et al. HyCAUSE Flight Test Program , 2008 .
[6] C R McClinton,et al. Airbreathing Hypersonic Technology Vision Vehicles and Development Dreams , 1999 .
[7] Aibing Yu,et al. Flow properties of particles in a model annular shear cell , 2012 .
[8] A. Roudakov,et al. CIAM/NASA Mach 6.5 Scramjet Flight and Ground Test , 1999 .
[9] Matthew Ringuette,et al. Coherent structures in direct numerical simulation of turbulent boundary layers at Mach 3 , 2007, Journal of Fluid Mechanics.
[10] Shihe Yi,et al. Supersonic flow imaging via nanoparticles , 2009 .
[11] Fulvio Scarano,et al. Three-dimensional instantaneous structure of a shock wave/turbulent boundary layer interaction , 2009, Journal of Fluid Mechanics.
[12] Yi Shihe,et al. Visualization of supersonic flow over double wedge , 2013 .