A standardized load sequence was derived by averaging the theoretical and experimental frequency distributions of loads on the wing roots of transport aircraft. The sequence is considered to be representative for the load history of the wing root of transport aircraft. It is proposed to adopt the standardized sequence for various aeronautical fatigue testing purposes.
A Standardized Load Sequence for Flight Simulation Tests on Transport Aircraft Wing Structures Standardisierter Einzelflug-Belastungsablauf fuer Schwingfestigkeitsversuche an Tragflaechenbauteilen von Transportflugzeugen
1973
58 pages
Report
Keine Angabe
Englisch
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