FLIGHT VIBRATION SURVEY OF C-133 AIRCRAFT

Abstract

A C-133A aircraft was surveyed to determine the vibration environment existing on the fuselage side-wall and the cargo deck under all normal flight conditions. Approximately 9,760 data points were obtained from 16 separate locations on the vehicle during three test flights. The data were evaluated to determine the adequacy of vibration testing requirements of the cargo area and will be used to arrive at a more realistic set of vibration test requirements concerning (1) items of cargo to be transported in such aircraft and (2) items of equipment which will be installed on the cargo deck or fuselage sidewalls of the C-133A.

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Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1962
Accession Number
AD0277128

Entities

People

  • Phyllis G. Bolds

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircraft Equipment
  • Aircrafts
  • Airframes
  • Environment
  • Fuselages
  • Vehicle Equipment
  • Vehicles
  • Vibration

Readers

  • Aerospace logistics and air mobility.
  • Explosive Engineering.
  • Software Engineering