Pressure Fluctuations Induced By a Hypersonic Turbulent Boundary Layer
Direct numerical simulations (DNS) are used to examine the pressure fluctuations generated by a spatially developed Mach 5.86 turbulent boundary layer. The unsteady pressure field is analysed at multiple wall-normal locations, including those at the wall, within the boundary layer (including inner layer, the log layer, and the outer layer), and in the free stream. The statistical and structural variations of pressure fluctuations as a function of wall-normal distance are highlighted. Computational predictions for mean-velocity profiles and surface pressure spectrum are in good agreement with experimental measurements, providing a first ever comparison of this type at hypersonic Mach numbers. The simulation shows that the dominant frequency of boundary-layer-induced pressure fluctuations shifts to lower frequencies as the location of interest moves away from the wall. The pressure wave propagates with a speed nearly equal to the local mean velocity within the boundary layer (except in the immediate vicinity of the wall) while the propagation speed deviates from Taylor's hypothesis in the free stream. Compared with the surface pressure fluctuations, which are primarily vortical, the acoustic pressure fluctuations in the free stream exhibit a significantly lower dominant frequency, a greater spatial extent, and a smaller bulk propagation speed. The free-stream pressure structures are found to have similar Lagrangian time and spatial scales as the acoustic sources near the wall. As the Mach number increases, the free-stream acoustic fluctuations exhibit increased radiation intensity, enhanced energy content at high frequencies, shallower orientation of wave fronts with respect to the flow direction, and larger propagation velocity.
L. Duan et al., "Pressure Fluctuations Induced By a Hypersonic Turbulent Boundary Layer," Journal of Fluid Mechanics, vol. 804, pp. 578-607, Cambridge University Press, Oct 2016.
The definitive version is available at https://doi.org/10.1017/jfm.2016.548
Mechanical and Aerospace Engineering
Center for High Performance Computing Research
Keywords and Phrases
Acoustic Wave Propagation; Acoustics; Aerodynamics; Atmospheric Thermodynamics; Boundary Layer Flow; Boundary Layers; Buoyancy; Mach Number; Turbulence; Turbulent Flow; Wavefronts; Computational Predictions; High Speed Flows; Mean Velocity Profiles; Propagation Velocities; Surface Pressure Fluctuations; Turbulence Simulation; Turbulent Boundary Layers; Unsteady Pressure Fields; Hypersonic Boundary Layers
International Standard Serial Number (ISSN)
Article - Journal
© 2016 Cambridge University Press, All rights reserved.
01 Oct 2016