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NASA NTRS · 20200010342

Shape Optimization of Vortex Generators to Control Mack Mode Amplification

Abstract

This 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.

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BibTeXRIS

Clark C Pederson, Meelan M Choudhari, Beckett Y Zhou, Pedro Paredes, Boris Diskin. 2020-06-08. Shape Optimization of Vortex Generators to Control Mack Mode Amplification. https://ntrs.nasa.gov/citations/20200010342

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