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

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.

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Document Details

Document Type
Technical Report
Publication Date
Jan 31, 1961
Accession Number
AD0257599

Entities

Organizations

  • General Motors

Tags

Communities of Interest

  • Air Platforms
  • Human Systems

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Air Force
  • Bending Moments
  • Boundary Layer
  • Controllable Pitch Propellers
  • Engineering
  • Engineers
  • Flow Fields
  • Government Procurement
  • Load Distribution
  • Mach Number
  • Propellers
  • Propulsion Systems
  • Systems Engineering
  • Turbines
  • Turboprop Engines
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Aerodynamics.
  • Aerospace Research.
  • Systems Analysis and Design