Calibration of a Strain-Gauged CT4-A Undercarriage.

Abstract

This memo presents the basic equations required to relate strains to components of flight and landing loads acting on CT4-A undercarriage legs. Details of strain gauge locations are contained in ARL Drawing No. 53432 and photographs and details of the test rig are included. The results of the calibration in February 1977 are recorded with details of the subsequent analysis. The application to flight test data is also described. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1980
Accession Number
ADA086965

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  • V. Romes

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  • Air Platforms
  • Space

DTIC Thesaurus Topics

  • Aerospace Industry
  • Air Force
  • Aircrafts
  • Analysis Of Variance
  • Bending Moments
  • Calibration
  • Deflection
  • Department Of Defense
  • Equations
  • Equations Of State
  • Flight Loads
  • Gages
  • Inboard
  • Information Science
  • Measurement
  • Strain Gages
  • Transverse

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