An approach to aerodynamic integration of turboprops and airframes, with emphasis placed upon wing mounted installations is addressed. Potential flow analytical techniques were employed to study aerodynamic integration of the prop fan propulsion concept with advanced, subsonic, commercial transport airframes. Three basic configurations were defined and analyzed: wing mounted prop fan at a cruise Mach number of 0.8, wing mounted prop fan in a low speed configuration, and aft mounted prop fan at a cruise Mach number of 0.8.
An analysis of prop-fan/airframe aerodynamic integration
01.10.1978
Report
Keine Angabe
Englisch
Analysis of Prop-Fan/Airframe Aerodynamic Integration
NTIS | 1978
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