Theoretical, Numerical, and Experimental Investigations of the Fundamental Processes That Drive Combustion Instabilities in Liquid Rocket Engines

Abstract

The objective of this research was to develop an integrated theoretical and computational framework for treating combustion dynamics of cryogenic and hydrocarbon propellants under conditions representative of contemporary liquid rocket engines.

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Document Details

Document Type
Technical Report
Publication Date
Sep 13, 2012
Accession Number
ADA568237

Entities

People

  • Ben T. Zinn
  • Chung K. Law
  • Ciprian Dumitrache
  • Hongfa Huo
  • John M. Quinlan
  • Martina Baroncelli
  • V. Akkerman
  • Vigor Yang
  • Xingjian Wang
  • Yong J. Kim

Organizations

  • Georgia Tech

Tags

Communities of Interest

  • Materials and Manufacturing Processes
  • Weapons Technologies

DTIC Thesaurus Topics

  • Abstracts
  • Acoustics
  • Combustion
  • Dynamics
  • Engineering
  • Engines
  • Governments
  • Information Operations
  • Instability
  • Rocket Engines
  • Rockets
  • Space Propulsion
  • Standards

Fields of Study

  • Physics

Readers

  • Combustion science or combustion engineering.
  • Military History / Militaries and War Studies