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Nonlinear Görtler Vortices and Their Secondary Instability in a Hypersonic Boundary LayerNonlinear development of the Görtler instability over a concave surface gives rise to a highly distorted inflectional flow field in the boundary layer that leads to both wall-normal and spanwise gradients in the flow. Such nonlinear structures are susceptible to strong, high-frequency secondary instabilities that may lead to the onset of laminar-turbulent transition. The present numerical study uses direct numerical simulations and linear secondary instability theory to investigate finite amplitude Görtler vortices and their secondary instability characteristics, respectively, in the hypersonic flow over an axisymmetric cone with a concave aft body. To complement previous studies in the literature wherein the Görtler instability was usually studied for a flat plate and initiated at some upstream location by imposing an eigenfunction as the inflow condition or by blowing and suction at the wall, the present investigation is focused on fully realizable Görtler instability that is excited by an azimuthally periodic array of surface protuberances. Furthermore, while the previous work had mostly focused on the secondary instability of Görtler vortices with cross-plane velocity contours that resembled bell-shaped structures, the present results confirm that fully developed mushroom structures also exist in the hypersonic regime when the Görtler vortex amplitude is sufficiently large. Computations further reveal that the dominant modes of secondary instability in these mushroom-shaped structures correspond to an antisymmetic (i.e., sinuous) “stem” mode that concentrates within the strong, nearly wall-normal internal shear layers surrounding the stem regions underneath the caps of the mushroom structures. Additionally, there exist a multitude of other significantly unstable secondary instability modes of both symmetric and antisymmetric types. Analogous to the secondary instability of crossflow vortices in hypersonic flows, secondary instability modes of both symmetric and antisymmetric types. Analogous to the secondary instability of crossflow vortices in hypersonic flows, secondary instability modes originating from the Mack mode instability play an important role during the nonlinear breakdown process.
Document ID
20200002646
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Fei Li
(Langley Research Center Hampton, Virginia, United States)
Meelan Choudhari ORCID
(Langley Research Center Hampton, Virginia, United States)
Pedro Paredes ORCID
(National Institute of Aerospace Hampton, Virginia, United States)
Date Acquired
April 17, 2020
Publication Date
June 14, 2019
Publication Information
Publication: AIAA Aviation 2019 Forum
Publisher: American Institute of Aeronautics and Astronautics
e-ISBN: 9781624105890
Subject Category
Aerodynamics
Report/Patent Number
NF1676L-31674
AIAA-2019-3216
Report Number: NF1676L-31674
Meeting Information
Meeting: AIAA AVIATION Forum and Exposition
Location: Dallas, TX
Country: US
Start Date: June 17, 2019
End Date: June 21, 2019
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
WBS: 725017.02.07.03.01
Distribution Limits
Public
Copyright
Use by or on behalf of the US Gov. Permitted.
Keywords
Laminar turbulent transition
Gortler vortices
Direct numerical simulation
Incompressible flow
Eigenfunction
Freestream Mach Number
Hypersonic wind tunnels
Adverse pressure gradient
Hypersonic speed
Velocity profiles
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