Three-Dimensional Simulations of a Gas/Gas, Hydrogen/Oxygen Engine

Abstract

Objectives: 1) Develop design tools and methodologies for rocket injectors. 2) Use experimental measurements to develop and anchor state-of-the-art flow codes. 3) Determine level of fidelity required to reasonably reproduce the essential physical behavior of a coaxial gas/gas injector flow.

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Document Details

Document Type
Technical Report
Publication Date
Dec 16, 2002
Accession Number
ADA410982

Entities

People

  • Mark R. Archambault
  • Oshin Peroomian

Organizations

  • Air Force Research Laboratory

Tags

Communities of Interest

  • Space

DTIC Thesaurus Topics

  • Abstracts
  • Air Force
  • Air Force Research Laboratories
  • Department Of Defense
  • Elements
  • Geometry
  • Hydrogen
  • Mathematics
  • Military Research
  • Physical Properties
  • Simulations
  • Sizes (Dimensions)
  • Three Dimensional

Fields of Study

  • Physics

Readers

  • Computational Modeling and Simulation
  • Internal Combustion Engine (ICE) Technology.