Wind Tunnel Test of the Conversion Process of a Folding Tilt-Rotor Aircraft Using a Semispan Unpowered Model. Volume 4. Part 2. Blade Stress Analysis, Bench Tests, and Wind Tunnel Model Details

Abstract

The document presents the detailed results of the blade stress analysis and the bench tests, as well as a description of the wind tunnel and the model. Mathematical findings are given in developed equations and in voluminous tabular data. Additional information is provided in the form of engineering graphs and curves, schematic diagrams, and photographs of the model and test setup. This volume is actually an appendix to Part I, Analysis and Results.

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Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1971
Accession Number
AD0735733

Entities

People

  • John Magee
  • Robert William Taylor

Organizations

  • Boeing Rotorcraft Systems

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Air Force
  • Air Force Facilities
  • Aircrafts
  • Angular Motion
  • Control Systems
  • Elastic Properties
  • Frequency
  • Geometry
  • Measurement
  • Mechanics
  • Modulus Of Elasticity
  • Research Facilities
  • Resonant Frequency
  • Test Facilities
  • Tilt Rotor Aircraft
  • Wind Tunnel Models
  • Wind Tunnels

Readers

  • Aerospace Engineering
  • Business Analytics
  • Fluid Dynamics.