Numerical Investigation of Interaction of Oblique Shock and Detonation Waves in a Steady Supersonic Flow of a Chemical Reactive Gaseous Mixture

Abstract

The main objective of the present work is to study the flow structure with reflection of oblique SW and DW in a steady supersonic flow of a chemically reacting mixture and the transition from regular to Mach reflection.

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Document Details

Document Type
Technical Report
Publication Date
Jul 01, 2002
Accession Number
ADA409142

Entities

People

  • A. N. Kudryavtsev
  • A. V. Trotsyuk
  • M. S. Ivanov

Organizations

  • Russian Academy of Sciences

Tags

Communities of Interest

  • Energy and Power Technologies
  • Materials and Manufacturing Processes

DTIC Thesaurus Topics

  • Applied Mechanics
  • Boundaries
  • Chemical Kinetics
  • Chemical Reactions
  • Computational Fluid Dynamics
  • Computational Science
  • Computations
  • Detonation Waves
  • Equations
  • Flow
  • Fluid Dynamics
  • Mach Number
  • Shock Waves
  • Supersonic Flow
  • Three Dimensional
  • Two Dimensional
  • Waves

Fields of Study

  • Physics

Readers

  • Fluid Mechanics and Fluid Dynamics.
  • Oceanography.
  • Rocket Propulsion.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers