Boundary layer transition in hypersonic boundary layer

【Author】

Chuanhong Zhang;Qing Tang;Cunbiao Lee;Yanji Hong;Jifei Ye;

【Abstract】

<正>High speed flow visualization,wall pressure measurement and PIV were used to study the transition of a cone and a flat plate boundary layer in our new established Mach 6 quiet tunnel.Quiet tunnel has much lower noise level of free stream(less than 0.1%). Experiments were conducted on a 5°-half-angle cone model and a flat plate.The flow visualizations showed the clear appearance and

【Keywords】

DNS;Boundary layer transition in hypersonic boundary layer;PIV;very;

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