Wing fatigue damage to aircraft was examined in regard to measurements made by peak-counting accelerometers. Major causes of damage were defined as repetitive stresses caused by ground loads, air loads and the ground-air-ground cycle. These phases of the aircraft loads environment were discussed in detail. Recommendations were made on the procedure for converting accelerometer data into loads spectra.
The Dissection of an Aircraft Loads Spectrum Produced by Peak-Counting Accelerometers
1977
24 pages
Report
Keine Angabe
Englisch
Accelerometers for determining aircraft flight loads
Engineering Index Backfile | 1952
|Design and use of counting accelerometers
TIBKAT | 1954
|