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
01.01.2002
Preprint
Keine Angabe
Englisch
NTRS | 2016
|NTRS | 2015
|NTRS | 2014
|Status of Nozzle Aerodynamic Technology at MSFC
NTRS | 2002
|