CH-46 Composite Rotor Blade Flight Stress Survey Data. Volume I,

Abstract

This document (13 volumes) presents plotted and tabulated flight data for all stress parameters measured during the CH-46 composite rotor blade flight stress survey and structural demonstration. This volume contains a description of test conditions, a summary of flight logs, calibrated blade section moduli and a complete description of instrumentation. The components under test were the A02R1702 composite rotor blades and the A02R1710 blade socket. Volumes 1 through 12 of this report contain the test results for the flight stress survey. Volume 13 contains the results of the structural demonstration.

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Document Details

Document Type
Technical Report
Publication Date
Jul 07, 1978
Accession Number
ADA075566

Entities

People

  • J. Bendo
  • R. Aiello

Organizations

  • Boeing Rotorcraft Systems

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Airspeed
  • Altitude
  • Batch Processing
  • Calibration
  • Center Of Gravity
  • Composite Materials
  • Demonstrations
  • Flight
  • Gravity
  • Instrumentation
  • Level Flight
  • Measuring Instruments
  • Operating Systems
  • Orientation (Direction)
  • Plastic Explosives
  • Stationary
  • Three Dimensional

Fields of Study

  • Physics

Readers

  • Aerodynamics.
  • Aerospace Test and Evaluation
  • Business Analytics