The Hot Section Technology (HOST) Project is a NASA-sponsored endeavor to improve the durability of advanced gas turbine engines for commercial and military aircraft. Through improvements in the analytical models and life prediction systems, designs for future hot section components, the combustor and turbine, will be more accurately analyzed and will incorporate features required for longer life in the more hostile operating environment of high performance engines.
Turbine Engine Hot Section Technology (HOST) Project
1986
6 pages
Report
Keine Angabe
Englisch
Structural Mechanics , Jet & Gas Turbine Engines , Combustion chambers , Engine parts , Gas turbine engines , High temperature , Operating temperature , Combustion temperature , Computerized simulation , Durability , Mathematical models , Nasa programs , Prediction analysis techniques , Service life
Turbine engine Hot Section Technology (HOST) project
NTRS | 1983
|Turbine Engine Hot Section Technology (HOST)
NTIS | 1982
Turbine Engine Hot Section Technology (HOST)
NTIS | 1983