Total Airframe Fatigue Test F 104 G

Abstract

The report contains the most important information and data on the experimental configuration, experimental sequence, and the results of the F 104 G total airframe fatigue experiment. Details are contained in 31 additional partial reports. In addition, the tables of Appendix B contain all the damage information which occurred on the structure during the experiments. This report can be used as a means of orientation for the information contained in the partial reports because of the cross references in the text and the tables.

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Document Details

Document Type
Technical Report
Publication Date
Mar 20, 1975
Accession Number
ADA007938

Entities

People

  • Schutz

Tags

Communities of Interest

  • Air Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aircrafts
  • Airframes
  • Crack Propagation
  • Eddy Currents
  • Fatigue Tests (Mechanics)
  • Fuselages
  • Materials
  • Measurement
  • Plastic Explosives
  • Sheet Metal
  • Spars
  • Strain Gages
  • Stress Analysis
  • Structural Components
  • Test And Evaluation
  • Test Methods
  • Time Intervals

Readers

  • Aerospace Engineering
  • Library and Information Science
  • Tribology (the study of the boundary interaction between sliding surfaces, lubrication, wear and friction).