Modeling the Surface Pressure Spectrum Beneath Turbulent Boundary Layers in Pressure Gradients

Author:

Fritsch Daniel J.,Vishwanathan Vidya,Roy Christopher J.,Todd Lowe K.,Devenport William J.,Croaker Paul,Tkachenko Oksana,Pook David,Lane Graeme1,Shubham Shubham,Sandberg Richard D.

Affiliation:

1. RMIT University, Melbourne, Victoria 3000, Australia

Abstract

A wide variety of models and methods for the prediction of the surface pressure spectrum beneath turbulent boundary layers is presented and assessed. A thorough review is made of the current state of the art in empirical and analytical pressure spectrum models; and predictions of zero, adverse, favorable, and nonequilibrium pressure gradient boundary layers are examined using a steady Reynolds-averaged Navier–Stokes (RANS) prediction of a subset of a pressure gradient boundary-layer benchmark flow case. The existing empirical models show either an inability to adapt to pressure gradient conditions or an oversensitivity to model inputs, producing nonphysical results under certain flow conditions. New empirical models are created using a gene expression programming machine-learning algorithm based on both experimental and RANS inputs. The various input options for analytical Toegepast Natuurwetenschappelijk Onderzoek (TNO) modeling are presented and assessed, and recommendations for best practices are made. The developed models show improvement in both accuracy and robustness over existing models.

Funder

Office of Naval Research Global

Office of Naval Research

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

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