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Accession Number:
AD0743968
Title:
Annealed Foil Fatigue Sensor Development
Corporate Author:
LOCKHEED-GEORGIA CO MARIETTA
Report Date:
1972-03-01
Abstract:
The development testing of the C-5A full-scale fatigue specimens presented a timely opportunity to continue the development of a system of fatigue sensing devices. The fatigue sensor selected for use was previously evaluated during an Air Force funded feasibility study and has been adapted to meet the application requirements on full-scale C-5A structure. The report constitutes the final report regarding this effort and applies specifically to an evaluation of the sensor on the C-5A laboratory fatigue test specimens. The techniques of sensor installation, location, data acquisition methods, and analysis of sensor response are herein evaluated in view of potential utilization on fleet aircraft.
Descriptive Note:
Final rept. Dec 1967-May 1971
Pages:
0231
Distribution Statement:
Approved for public release; distribution is unlimited.
Contract Number:
F33615-68-C-1221
File Size:
31.82MB
