Accession Number:

AD0257599

Title:

FINAL DESIGN ANALYSES OF AF 205F-272. PART 1. PROPELLER AT TIME OF FIRST RUN

Descriptive Note:

Corporate Author:

GENERAL MOTORS CORP INDIANAPOLIS IN ALLISON GAS TURBINE DIV

Personal Author(s):

Report Date:

1961-01-31

Pagination or Media Count:

38.0

Abstract:

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.

Subject Categories:

  • Aircraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE