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.
Descriptors:
Subject Categories:
- Attack and Fighter Aircraft