Efficient global resolvent analysis via the one-way Navier-Stokes equations. Part 2. Optimal response

TL;DR

This paper introduces an efficient spatial marching approach using the one-way Navier-Stokes equations to compute resolvent modes, significantly reducing computational costs for flow response analysis in complex aerodynamic problems.

Contribution

It develops a novel adjoint-based optimization method leveraging OWNS for fast resolvent mode approximation, bypassing global discretization bottlenecks.

Findings

Validated method on supersonic jet and boundary layer flows.

Achieved comparable results to global calculations with reduced computational effort.

Demonstrated effectiveness for high Mach number turbulent flows.

Abstract

In this study, we develop an efficient approach for approximating resolvent modes via spatial marching. Building on the methodology from Part 1, we leverage the ability of the projection-based formulation of the one-way Navier-Stokes equations (OWNS) to efficiently and accurately approximate the downstream response of the linearized Navier-Stokes equations to forcing for problems containing a slowly varying direction. Using an adjoint-based optimization framework, forcings that optimally excite a response in the flow are computed by marching the forward and adjoint OWNS equations in the downstream and upstream directions, respectively. This avoids the need to solve direct and adjoint globally-discretized equations, therefore bypassing the main computational bottleneck of a typical global resolvent calculation. The method is demonstrated for a supersonic turbulent jet at Mach 1.5 and a transitional zero-pressure-gradient flat-plate boundary layer flow at Mach 4.5, and the optimal OWNS results are validated against corresponding global calculations.