Occurrence of global instability in hypersonic compression corner flow

• Published in: Journal of fluid mechanics Vol. 919
• Main Authors: Hao, Jiaao, Cao, Shibin, Wen, Chih-Yung, Olivier, Herbert
• Format: Journal Article
• Language: English
• Published: Cambridge, UK Cambridge University Press 25.07.2021
• Subjects: Angles (geometry); Compression; Computational fluid dynamics; Corner flow; Dimensional stability; Experiments; Flow separation; Flow stability; Flow system; Fluid flow; Fluid mechanics; Heat; Hypersonic flow; Instability; JFM Papers; Mach number; Perturbation; Reynolds number; Separation; Simulation; Stability analysis; Temperature; Three dimensional analysis; Triple-deck theory; Two dimensional flow; Vortices; Wall temperature; Aachen Germany; Germany; hypersonic flow; boundary layer separation; absolute/convective instability
• ISSN: 0022-1120; 1469-7645
• DOI: 10.1017/jfm.2021.372

Hypersonic flow over a two-dimensional compression corner with a Mach number of 7.7 and unit Reynolds number of 4.2 × 106 m−1 is numerically investigated. Special emphasis is given to the onset of global instability with respect to three-dimensional perturbations. Global stability analysis is performed for various ramp angles and wall temperatures. It is found that the shock-induced separated flow system becomes unstable when the ramp angle is beyond a certain value. The critical ramp angle increases slightly with the wall temperature, although the length of the separation region is significantly enlarged. The global instability is shown to be closely linked with the occurrence of secondary separation beneath the primary separation bubble. A criterion is established based on a scaled ramp angle defined in the triple-deck theory to predict the global stability boundary, which depends on the free-stream conditions and geometries only.