NASA NTRS · 19900058269
Fatigue life estimates for helicopter loading spectra
Abstract
Helicopter loading histories applied to notch metal samples are used as examples, and their fatigue lives are calculated by using a simplified version of the local strain approach. This simplified method has the advantage that it requires knowing the loading history in only the reduced form of ranges and means and number of cycles from the rain-flow cycle counting method. The calculated lives compare favorably with test data.
Keep this discovery
Explore connections, maps & timelines
Khosrovaneh, A. K., Dowling, N. E., Berens, A. P., Gallagher, J. P.. 1990-07-01. Fatigue life estimates for helicopter loading spectra. https://ntrs.nasa.gov/citations/19900058269
Cite the original work for its findings. Save a collection to share your selection of sources.