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
No indication
English
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
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