Rocket Combustion Modelling Test Case RCM-3. Numerical Calculation of MASCOTTE 60 bar Case with THESEE

Abstract

This paper presents the numerical simulation of the RCM-3 test case done by Snecma and LCSR. The specified inlet conditions and computational options are described in the paper. A brief discussion about the main results is also given.

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 2001
Accession Number
ADP012372

Entities

People

  • A. Depoutre
  • D. Saucereau
  • E. Bodele
  • I. Gokalp
  • J. P. Dumont
  • S. Zurbach

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Atomization
  • Chambers
  • Chemical Reactions
  • Combustion
  • Combustion Chambers
  • Computational Fluid Dynamics
  • Experimental Data
  • Flames
  • Heat Energy
  • Heat Of Vaporization
  • Heat Transfer
  • Ideal Gas Law
  • Liquid Oxygen
  • Payload
  • Simulations
  • Thermodynamic Properties
  • Thermodynamics

Readers

  • Computational Fluid Dynamics (CFD)
  • Criminal Law