This document presents the installed engine performance for a family of parametric engines of consistent technology developed to support production supersonic transport studies evaluating the effect of engine cycle on noise and airplane performance. (Author)
SST Parametric Engine Library - Installed Engine Performance
1971
253 pages
Report
Keine Angabe
Englisch
Jet & Gas Turbine Engines , Aircraft , Turbofan engines , Turbojet engines , Jet transport planes , Supersonic aircraft , Design , Supersonic flight , High altitude , Subsonic flow , Low altitude , Jet engine noise , Reduction , Afterburners , Fuel consumption , Rotary compressors , Pressure , Variable area nozzles , Exhaust nozzles , Drag , Turbojet inlets , Nozzle throats , Weight , Installation , Performance(Engineering) , Thrust , Thrust augmentation , Bleed systems , Takeoff , Afterburning , Mathematical prediction , Mathematical models , Simulation , Ge-4 engines , Jtf-17 engines , Supersonic transports , Boattails , Computer aided design , Turbofan inlets
INSTALLED PERFORMANCE OF THE TF39 ENGINE
SAE Technical Papers | 1969
|Installed Outdoor Engine Testing
SAE Technical Papers | 2007
Installed Outdoor Engine Testing
SAE Technical Papers | 2023
Trans Tech Publications | 2013
|Installed engine performance in dust-laden atmosphere
AIAA | 1984
|