A low pressure oxygen/hydrogen turbine drive combustor hot-fire test series was conducted on the Turbine Drive Combustor Technology Program. The first objective was to gather data on an axisymmetric combustion system to support anchoring of a new combustion/fluid dynamics computer code under development on the same contract. The second objective was to gain insight into low mixture ratio combustion characteristics of coaxial injector elements.
Laser Schlieren and ultraviolet diagnostics of rocket combustion
01.04.1985
Aufsatz (Konferenz)
Keine Angabe
Englisch
A Quantitative Analysis of Schlieren Photography for an Internal Combustion Engine Diagnostics
SAE Technical Papers | 1991
|A quantitative analysis of schlieren photography for an internal combustion engine diagnostics
Kraftfahrwesen | 1991
|Rocket Combustion Diagnostics by Laser Induced Breakdown Spectroscopy AIAA Paper
British Library Conference Proceedings | 2007
|