Rotor Loads Prediction: A Matched-Harmonic Confluence Approach, with Application to 600+ UH-60A Flight Counters

This effort focuses on application of the Load Confluence Algorithm (LCA) to the analysis of a large set of flight test data from the NASA/US Army UH-60A Airloads Program. In order to show the robustness of the LCA in the context of a structural health monitoring program, over 600 flight counters have been examined, covering the full range of speeds, weights, thrust settings, and maneuvers for that test program.