Wall heat flux in supersonic turbulent expansion flow with shock impingement

Abstract

We perform direct numerical simulations to investigate the characteristics of wall heat flux (WHF) in the interaction of an oblique shock wave at an angle of 33.2° and free-stream Mach number M_∞ = 2.25 impinging on supersonic turbulent expansion corners with deflection angles of 0^o (flat plate), 6^o and 12^o. The effect of the expansion on the WHF characteristics is analysed by comparing it to the interaction with the flat plate under the same flow conditions and a fixed shock impingement point. In the post-expansion region, the decreased mean WHF is found to collapse onto the flat plate case when scaled with the mean wall pressure. The statistical properties of the WHF fluctuations, including probability density function, frequency spectra, and space–time correlations, are comparatively analysed. The expansion causes an increase in the occurrence probability of negative extreme events, an enhancement of high-frequency energy, and an inhibition of intermediate-frequency energy. The increased expansion angle also results in a faster recovery of characteristic spanwise length scales and an increase in convection velocity. We use the mean WHF decomposition method in conjunction with bidimensional empirical mode decomposition to quantitatively analyse the impact of expansion on scale contributions. It is demonstrated that the presence of the expansion corner has no significant impact on the decomposed results, but it significantly reduces the contribution associated with outer large-scale structures.

KEYWORDS:

• Expansion corner
• turbulent boundary layer
• shock impingement
• wall heat flux

Disclosure statement

No potential conflict of interest was reported by the author(s).

Additional information

Funding

This study was co-supported by the National Key R&D Program of China (No. 2019YFA0405300) and the National Natural Science Foundation of China (No. 11972356).