Prediction of resolvent mode shapes in supersonic turbulent boundary layers

Document Details

Document Type
Pub Defense Publication
Publication Date
Oct 01, 2020
Source ID
10.1016/j.ijheatfluidflow.2020.108677

Entities

People

  • Beverley McKeon
  • Scott T.m. Dawson

Organizations

  • Air Force Office of Scientific Research

Tags

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers
  • Hypersonics - Hypersonic Flow