Boundary layer transition in hypersonic boundary layer


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


<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


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


To explore the background and basis of the node document

Springer Journals Database

Total: 0 articles

Similar documents

Documents that have the similar content to the node document