Accession Number:

ADA439189

Title:

Hydrocarbon-Fueled Scramjet Research at Hypersonic Mach Numbers

Descriptive Note:

Final rept. 1 Feb 2002-31 Mar 2003

Corporate Author:

AUSTRALIAN NATIONAL UNIV CANBERRA DEPTOF PHYSICS

Personal Author(s):

Report Date:

2005-03-31

Pagination or Media Count:

138.0

Abstract:

Planar laser-induced fluorescence PLIF of OH and wall-pressure measurements have been used to investigate the combustion in a cavity flame-holder scramjet combuster.

Subject Categories:

  • Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE