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Film cooling of accelerated flow in a subscale combustion chamber
R. Arnold, D. Suslov,
O. J. Haidn
Deutsches Zentrum für Luft- und Raumfahrt (DLR)
Institute of Space Propulsion
Research output
:
Contribution to journal
›
Article
›
peer-review
35
Scopus citations
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Keyphrases
Combustion Chamber
100%
Accelerating Flow
100%
Film Cooling
100%
Rocket Combustor
50%
Hot Gas
50%
High Performance
25%
Pressure Level
25%
Combustion Chamber Pressure
25%
Temperature Distribution
25%
Combustion Pressure
25%
Blowing Rate
25%
Film Blowing
25%
Copper Liner
25%
Axial Distribution
25%
Nozzle Segment
25%
Cooling Model
25%
Engineering
Combustion Chamber
100%
Hot Gas
40%
Pressure Level
20%
Chamber Pressure
20%
Experimental Investigation
20%
Convergent
20%
Convective
20%
Film Blowing
20%
Blowing Rate
20%
Initial Temperature
20%
Physics
Combustion Chamber
100%
Film Cooling
100%
High Temperature Gas
40%
Supersonics
20%