Acoustic receptivity of compressible Tollmien-Schlichting waves with an efficient time-harmonic linearized Navier-Stokes method
File(s)acoustic-receptivity-raposo.pdf (457.12 KB)
Accepted version
Author(s)
Raposo, H
Mughal, MS
Ashworth, R
Type
Conference Paper
Abstract
The compressible formulation of the time-harmonic linearized Navier-Stokes (LNS) method
for acoustic receptivity prediction is described. The efficiency of the proposed approach
is rooted in the assumption that the problems of interest only require the time-asymptotic
solution of a few select frequencies. We explore the parabolic nature of the basic flow and of the
Stokes layer, and we implement an efficient LU decomposition method to obtain the roughness-
induced steady perturbation and Tollmien-Schlichting wave. Before attempting to predict
receptivity amplitudes, the compressible Stokes layer solution based on the linearized unsteady
boundary layer equations is validated in the subsonic regime against an Orr-Sommerfeld-type
equation. Further testing of the model is conducted by reproducing the experiments of King
&
Breuer in near incompressible conditions. The results are consistent with the analogue
incompressible receptivity model, and reveal excellent agreement with finite-Reynolds number
theory for two-dimensional instabilities. Qualitative agreement with the experimental results
for oblique waves is observed. Differences can be partially explained by the choice of physical
model used to determine the N-factors, which in turn are used to extrapolate amplitudes to
the first-branch of stability. Ultimately, a comprehensive comparison with direct-numerical-
simulation-based subsonic receptivity amplitudes is conducted, demonstrating the correctness
of the mathematical model and numerical implementation described herein.
for acoustic receptivity prediction is described. The efficiency of the proposed approach
is rooted in the assumption that the problems of interest only require the time-asymptotic
solution of a few select frequencies. We explore the parabolic nature of the basic flow and of the
Stokes layer, and we implement an efficient LU decomposition method to obtain the roughness-
induced steady perturbation and Tollmien-Schlichting wave. Before attempting to predict
receptivity amplitudes, the compressible Stokes layer solution based on the linearized unsteady
boundary layer equations is validated in the subsonic regime against an Orr-Sommerfeld-type
equation. Further testing of the model is conducted by reproducing the experiments of King
&
Breuer in near incompressible conditions. The results are consistent with the analogue
incompressible receptivity model, and reveal excellent agreement with finite-Reynolds number
theory for two-dimensional instabilities. Qualitative agreement with the experimental results
for oblique waves is observed. Differences can be partially explained by the choice of physical
model used to determine the N-factors, which in turn are used to extrapolate amplitudes to
the first-branch of stability. Ultimately, a comprehensive comparison with direct-numerical-
simulation-based subsonic receptivity amplitudes is conducted, demonstrating the correctness
of the mathematical model and numerical implementation described herein.
Date Issued
2018-06-25
Date Acceptance
2018-06-01
Citation
2018 Fluid Dynamics Conference, AIAA AVIATION Forum, 2018
Publisher
AIAA
Journal / Book Title
2018 Fluid Dynamics Conference, AIAA AVIATION Forum
Copyright Statement
© 2018 by Airbus Group Ltd.. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission.
Sponsor
Engineering and Physical Sciences Research Council
Innovate UK
Identifier
https://arc.aiaa.org/doi/abs/10.2514/6.2018-3379
Grant Number
EP/I037946/1
113022
Source
2018 Fluid Dynamics Conference
Publication Status
Published
Start Date
2018-06-25
Finish Date
2018-06-29
Coverage Spatial
Atlanta, Georgia
Date Publish Online
2018-06-27