CH-46 Composite Rotor Blade Flight Stress Survey Data. Volume IX. Tabulated Forward Rotor Blade Angles and Loads,

Abstract

This volume contains measured steady and alternating forward rotor blade angles and loads tabulated by flight and event number. In addition, the associated maximum and minimum forward flap angles are also included. The steady and alternating data is plotted versus true airspeed and can be found in Volumes 2 and 3.

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1978
Accession Number
ADA075618

Entities

People

  • J. Bendo
  • R. Aiello

Organizations

  • Boeing Rotorcraft Systems

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Abstracts
  • Aircrafts
  • Airspeed
  • Composite Materials
  • Flight Loads
  • Gages
  • Helicopters
  • Identification
  • Instrumentation
  • Materials
  • Measuring Instruments
  • Plastic Explosives
  • Strain Gages
  • Test Facilities
  • Three Dimensional
  • Two Dimensional

Fields of Study

  • Agricultural and Food sciences
  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Aerospace Engineering
  • Business Analytics