FINAL DESIGN ANALYSES OF AF 205F-272. PART 1. PROPELLER AT TIME OF FIRST RUN
GENERAL MOTORS CORP INDIANAPOLIS IN ALLISON GAS TURBINE DIV
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Design analyses, propeller description, structural analysis including performance considerations, aerodynamic design analysis, and a weight breakdown of the AF 205F-272 propeller configuration at the time of the first run are presented. This report is intended to present information which ill lend itself directly to the final design configuration of a controllable pitch propeller.