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Shape Optimization of Vortex Generators to Control Mack Mode AmplificationThis paper demonstrates the potential to use shape optimization for the design of vortex generators in an axisymmetric boundary layer. This shape optimization increases the amplitude of stationary streaks created by streamwise vorticity, with the goal of reducing the amplification of Mack mode instabilities. The test case under consideration matches a trajectory point during the ascent phase of the HIFiRE-1 flight experiment. Wall-mounted vortex generators are added to the cone and their shape is optimized to control the amplification of Mack mode instabilities that are known to initiate laminar-turbulent transition in this flow. An empirical objective function is developed based on the previous studies of optimal streaks. A constraint on the maximum streak amplitude is added to avoid the initiation of bypass transition. The shape optimization is conducted using SU2, an open-source suite for multiphysics simulation and design. A significant improvement is observed in an integral metric of the streak amplitude, while the maximum streak amplitude is maintained close to the baseline level. The qualitative features of the optimized geometry are discussed.
Document ID
20200010342
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Clark C Pederson
(The University of Texas at Austin Austin, Texas, United States)
Meelan M Choudhari ORCID
(Langley Research Center Hampton, Virginia, United States)
Beckett Y Zhou ORCID
(University of Kaiserslautern Kaiserslautern, Rheinland-Pfalz, Germany)
Pedro Paredes ORCID
(National Institute of Aerospace Hampton, Virginia, United States)
Boris Diskin
(National Institute of Aerospace Hampton, Virginia, United States)
Date Acquired
May 19, 2020
Publication Date
June 8, 2020
Publication Information
Publication: AIAA AVIATION 2020 Forum
Publisher: American Institute of Aeronautics and Astronautics
e-ISBN: 9781624105982
Subject Category
Aerodynamics
Report/Patent Number
NF1676L-34831
AIAA-2020-2963
Meeting Information
Meeting: AIAA AVIATION Forum and Exposition
Location: Virtual
Country: US
Start Date: June 15, 2020
End Date: June 19, 2020
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
WBS: 725017.02.07.03.01
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Keywords
Vortex generators
Shape optimization
Laminar turbulent transition
Tollmien Schlichting waves
Direct numerical simulation
Freestream Mach Number
Sequential quadratic programming
Hypersonic flows
Navier Stokes equations
Lagrange multipliers
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