A Preliminary Investigation of Nomad Instrumentation Boom Vibration.

Abstract

An investigation of the lower order modes of vibration of an instrumentation boom fitted to a Nomad aircraft was carried out and the results are presented. Recommendations for reducing the amplitude of boom vibration experienced at take-off are made. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Feb 01, 1978
Accession Number
ADA055010

Entities

People

  • B. Quinn
  • P. A. Farrell

Tags

DTIC Thesaurus Topics

  • Accelerometers
  • Air Force
  • Aircrafts
  • Amplitude
  • Australia
  • Carbon Fibers
  • Department Of Defense
  • Frequency
  • Fuselages
  • Instrumentation
  • Materials
  • Mechanical Impedance
  • Nose Wheels
  • Noses
  • Resonant Frequency
  • Stiffening
  • Vibration

Readers

  • Aerospace Test and Evaluation
  • Atmospheric Remote Sensing.
  • Aviation Science / Aeronautics.