4.5 Article

Improved nonlinear parabolized stability equations approach for hypersonic boundary layers*

Journal

CHINESE PHYSICS B
Volume 30, Issue 5, Pages -

Publisher

IOP PUBLISHING LTD
DOI: 10.1088/1674-1056/abd2a3

Keywords

nonlinear parabolized stability equations (NPSEs); hypersonic boundary layers; streamwise wavenumber

Funding

  1. National Natural Science Foundation of China [12072232, 11672351]
  2. National Key Project of China [GJXM92579]

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The study discusses the use of the nonlinear parabolized stability equations (NPSEs) approach to analyze disturbances in hypersonic boundary layers, proposing two improvements to address the divergence issue that may occur due to strong nonlinear effects or when dominant waves no longer play a leading role. By categorizing disturbances into dominant and non-dominant waves, and employing different methods to calculate streamwise wavenumbers, the improved NPSEs approach exhibits greater robustness compared to the traditional approach.
The nonlinear parabolized stability equations (NPSEs) approach is widely used to study the evolution of disturbances in hypersonic boundary layers owing to its high computational efficiency. However, divergence of the NPSEs will occur when disturbances imposed at the inlet no longer play a leading role or when the nonlinear effect becomes very strong. Two major improvements are proposed here to deal with the divergence of the NPSEs. First, all disturbances are divided into two types: dominant waves and non-dominant waves. Disturbances imposed at the inlet or playing a leading role are defined as dominant waves, with all others being defined as non-dominant waves. Second, the streamwise wavenumbers of the non-dominant waves are obtained using the phase-locked method, while those of the dominant waves are obtained using an iterative method. Two reference wavenumbers are introduced in the phase-locked method, and methods for calculating them for different numbers of dominant waves are discussed. Direct numerical simulation (DNS) is performed to verify and validate the predictions of the improved NPSEs in a hypersonic boundary layer on an isothermal swept blunt plate. The results from the improved NPSEs approach are in good agreement with those of DNS, whereas the traditional NPSEs approach is subject to divergence, indicating that the improved NPSEs approach exhibits greater robustness.

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