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Energy transfer of hypersonic and high-enthalpy boundary layer instabilities and transition
Phys. Rev. Fluids 7, 033901 – Published 8 March, 2022
DOI: https://doi.org/10.1103/PhysRevFluids.7.033901
Abstract
In this study, the disturbance energy budget is analyzed on the derived disturbance energy norm in hypersonic and high-enthalpy boundary layers with thermal-chemical nonequilibrium (TCNE) effects. The disturbance growth rate is decomposed to quantitatively evaluate the contribution from various classified terms. Hypersonic flat-plate flows are investigated with various free-stream Mach numbers, free-stream temperatures, and wall temperatures. The linear and nonlinear evolutions of disturbances are predicted using linear stability theory and parabolized stability equations. The results show that in the first-mode region, the disturbance growth rates are determined by the production term (destabilizing) and the viscous term (stabilizing), while the former nearly offset the latter. In the second-mode region, the viscous term decreases to the minimum, resulting in the dominance of the second mode. The disturbance of the TCNE source term has a stabilizing effect on the second mode, but at most it reduces the growth rate by in a Mach 10 adiabatic case with the highest free-stream temperature of . The production term is mainly responsible for the second-mode growth rate difference between the TCNE flow and calorically perfect gas flow. TCNE changes the disturbance characteristics mainly through the mean flow modification. In the oblique-mode breakdown case, the intensive energy transfer between the selected modes and their harmonic waves is found to occur where they interact strongly with the mean flow.
Physics Subject Headings (PhySH)
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