DLR Portal
Home|Textversion|Imprint|Sitemap|Contact Imprint Privacy |Deutsch
You are here: Home:Departments and Groups:Gas Turbines
Advanced Search
Key Research Topics
Departments and Groups
Chemical Kinetics and Analytics
Computer Simulation
Gas Turbines
Combustion Diagnostics
Multiphase Flow and Alternative Fuels
High-pressure Experiments
Research Facilities
Projects
Publications
Job Opportunities
Press Release
How to find us

Back to article

OH* Chemiluminescence images at air/fuel ratios of 1.85 (left), 2.7 (centre) and 3.1 (right) of a FLOX® based combustion system with 20 nozzles at a preheating temperature of 580 degrees Celsius.



1/2 Next
OH* Chemiluminescence images at air/fuel ratios of 1.85 (left), 2.7 (centre) and 3.1 (right) of a FLOX® based combustion system with 20 nozzles at a preheating temperature of 580 degrees Celsius.
OH* Chemiluminescence images at air/fuel ratios of 1.85 (left), 2.7 (centre) and 3.1 (right) of a FLOX® based combustion system with 20 nozzles at a preheating temperature of 580 degrees Celsius.
Research Fields
2019
Combustion systems for micro gas turbines
Micro gas turbine-based power plants
Numerical Cycle Simulations
Research Facilities
ATM Lab
Research Power Plant - MGT
Test Centre - MGT
Related Topics
Combustible
Dependability
Lasers and Masers
Copyright © 2021 German Aerospace Center (DLR). All rights reserved.