The application of new aerodynamic, structural, and propulsion technologies to a specified baseline commuter aircraft is studied. The assessment models can be used on a desktop calculator and include a sizing program, operating cost program, and passenger ride qualities model. Evaluation is done with a step-by-step approach and is applied to range, number and type of engines, structure, wing selection, and configuration. A 40 percent direct operating cost saving is anticipated compared to current well established commuter aircraft.
Advanced technologies applied to reduce the operating costs of small commuter transport aircraft
International Council of the Aeronautical Sciences ; 1982 ; Seattle, WA
1982-01-01
Miscellaneous
No indication
English
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