numerical solution for inviscid supersonic flow
High temperature instantaneous supersonic flow measurement using hydroxyl tagging velocimetry
Flow visualization of supersonic flow around a concave optical bow cap model of warhead
Aerodynamic flutter and limited cycle of a 2-D wing in the supersonic flow field
Study of density field measurement based on NPLS technique in supersonic flow
Nonlinear thermal flutter response of two dimensional panels in supersonic flow
Investigation of detached detonation induced by oblique shock in premixed supersonic flow
Since supersonic phenomena seldom occur naturally, the first studies of supersonic flow and flight were related to artifacts, from shells to turbines, rockets, and aircraft.
The ellipse arc may depress the acceleration of supersonic flow in inlet area, decrease the strength of inlet shock wave.
The experimental results show that the higher the static temperature and the density ratio between two supersonic flow, the more the total pressure losses of flow during mixing.
