Capability to optimize for turbine performance and accurately predict unsteady loads will allow for increased reliability, Isp, and thrust-to-weight. The development of a fast, accurate, validated aerodynamic design, analysis, and optimization system is required.
MSFC Turbine Performance Optimization (TPO) Technology Verification Status
JANNAF 26th Airbreathing Propulsion Subcommittee Meeting ; 2002 ; Destin, FL, United States
2002-01-01
Preprint
No indication
English
NTRS | 2016
|NTRS | 2015
|NTRS | 2014
|Status of Nozzle Aerodynamic Technology at MSFC
NTRS | 2002
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