Fully Coupled Nonlinear Aerothermoelastic Computational Model of a Plate in Hypersonic Flow

Document Details

Document Type
Pub Defense Publication
Publication Date
Jul 01, 2021
Source ID
10.2514/1.j060085

Entities

People

  • Earl H. Dowell
  • Maxim Freydin

Organizations

  • Air Force Office of Scientific Research
  • Duke University
  • Technion – Israel Institute of Technology

Tags

Technology Areas

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