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

Abstract

This volume contains measured steady and alternating aft rotor blade angles and loads tabulated by flight and event number. In addition, the associated maximum and minimum aft flap angles are also included. The steady and alternating data is plotted versus true airspeed and can be found in Volumes 4 and 5.

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1978
Accession Number
ADA075619

Entities

People

  • J. Bendo
  • R. Aiello

Organizations

  • Boeing Rotorcraft Systems

Tags

Communities of Interest

  • C4I

DTIC Thesaurus Topics

  • Airspeed
  • Composite Materials
  • Flight Loads
  • Gages
  • Helicopters
  • Identification
  • Instrumentation
  • Measurement
  • Rain Gages
  • Sequences
  • Test Facilities
  • Three Dimensional
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Aerospace Engineering
  • Business Analytics
  • Geodesy