A standardized load sequence for flight simulation tests on transport aircraft wing structures

A description is given of the development of a standardized load sec[uence which may be considered to be representative for the load history of the wing root of transport aircraift. It is proposed to adopt this standardized sequence for various aeronautical fatigue testing purposes. The standardization proposal was jointly developed by Laboratorium fur Betriebsfestigkeit, Darmstadt, German Federal Republic, and the National Aerospace Laboratory NLR; The Netherlands