Circa 1990 propulsion improvement concepts are discussed for 1000 to 5000 SHP conventional turboprop powerplants including engines, gearboxes, and propellers. Cycle selection, power plant configurations and advanced technology elements are defined and evaluated using average stage length DOC for commuter aircraft as the primary merit criterion.
Propulsion opportunities for future commuter aircraft
1982-01-01
Aufsatz (Konferenz)
Keine Angabe
Englisch
Propulsion Opportunities for Future Commuter Aircraft
NTIS | 1982
|Propulsion opportunities for future commuter aircraft
NTRS | 1982
|Propulsion opportunities for future commuter aircraft
AIAA | 1982
|Future Propulsion Opportunities for Commuter Airplanes
NTRS | 1982
|Future Propulsion Opportunities for Commuter Airplanes
SAE Technical Papers | 1982
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