A Lagrange multiplier-based optimal control technique for streak attenuation in high-speed boundary layers
Omar Es-Sahli, Adrian Sescu, M. Z. A. Koshuriyan, Yuji Hattori, Makoto, Hirota

TL;DR
This paper develops a Lagrange multiplier-based optimal control method to suppress vortex growth in high-speed boundary layers, reducing transition to turbulence and improving flow stability in supersonic and hypersonic flows.
Contribution
It introduces a novel optimal control algorithm using Lagrange multipliers applied to compressible boundary layer equations for vortex attenuation.
Findings
Significant reduction in kinetic energy of vortices
Decreased wall shear stress in controlled flows
Flattening of vortex instabilities spanwise
Abstract
High-amplitude free stream turbulence and surface roughness elements can excite a laminar boundary layer flow sufficiently to cause streamwise oriented vortices to develop. These vortices resemble elongated streaks having alternate spanwise variations of the streamwise velocity. Downstream, the vortices `wobble' through an inviscid secondary instability mechanism and, ultimately, transition to turbulence. We formulate an optimal control algorithm to suppress the growth rate of the streamwise vortex system. Considering a high Reynolds number asymptotic framework, we reduce the full compressible Navier-Stokes equations to the nonlinear compressible boundary region equations (NCBRE). We then implement the method of Lagrange multipliers via an appropriate transformation of the original constrained optimization problem into an unconstrained form to obtain the disturbance equations in the…
Peer Reviews
No public reviews on file for this paper yet. If you reviewed it on a platform where reviews are public (OpenReview, ICLR, NeurIPS, ICML), you can paste yours below so the community can read it here.
Videos
No videos yet. Explain this paper in a talk, walkthrough, or lecture? Add one.
Taxonomy
TopicsFluid Dynamics and Turbulent Flows · Computational Fluid Dynamics and Aerodynamics · Plasma and Flow Control in Aerodynamics
