Accession Number:

ADA007938

Title:

Total Airframe Fatigue Test F 104 G

Descriptive Note:

Final rept.

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSONAFB OH

Personal Author(s):

Report Date:

1975-03-20

Pagination or Media Count:

109.0

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.

Subject Categories:

  • Attack and Fighter Aircraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE