Nozzle Geometry Effects on Corner Boundary Layers in Supersonic Wind Tunnels

Document Details

Document Type
Pub Defense Publication
Publication Date
Aug 01, 2019
Source ID
10.2514/1.j058310

Entities

People

  • Holger Babinsky
  • Kshitij Sabnis

Organizations

  • Air Force Office of Scientific Research
  • University of Cambridge

Tags

Technology Areas

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