Test Case RCM-3 Using CPS

Abstract

The test case RCM-3 consists of modeling the MASCOTTE combustor at a pressure chamber of 60 bar, which is higher than the critical pressure of liquid oxygen (50.4 bar). This range of pressure is thought to be representative of the chamber pressure encountered in real engine. The CPS code (version 1.3) was used to model this test case. Various models have been compared between them and to the experimental results available.

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 2001
Accession Number
ADP012370

Entities

People

  • B. Legrand
  • P. Durand
  • P. Vuillermoz

Organizations

  • CNES

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Chambers
  • Combustion
  • Computational Fluid Dynamics
  • Critical Temperature
  • Emission
  • Gas Laws
  • Heat Transfer
  • Injectors
  • Liquid Oxygen
  • Near Field
  • Payload
  • Physical Properties
  • Surface Tension
  • Technical Information Centers
  • Thermodynamics
  • Turbulence

Fields of Study

  • Physics

Readers

  • Computational Modeling and Simulation
  • Petroleum Engineering
  • Structural Dynamics.