Accession Number:

ADP012372

Title:

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

Descriptive Note:

Corporate Author:

SOCIETY NATIONAL D'ETUDE ET DE CONSTRUCTION DE MOTEURS D'AVIATION MOISSY-CRAMAYEL (FRANCE)

Report Date:

2001-03-01

Pagination or Media Count:

11.0

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.

Subject Categories:

  • Computer Programming and Software
  • Combustion and Ignition

Distribution Statement:

APPROVED FOR PUBLIC RELEASE