Nonequilibrium Dissociation and Recombination Models for Hypersonic Flows

Document Details

Document Type
Pub Defense Publication
Publication Date
May 01, 2022
Source ID
10.2514/1.j061154

Entities

People

  • Narendra Singh
  • Thomas E. Schwartzentruber

Organizations

  • Air Force Office of Scientific Research
  • Stanford University
  • University of Minnesota

Tags

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flight