Abstract: A computer-implemented method for applying passive strain indicators to a component includes creating a plurality of surface curves and a plurality of data points on each of the plurality of surface curves, the plurality of surface curves and the plurality of data points defining the exterior surface of the component. The method further includes receiving data indicative of a user input selection of a selected surface curve of the plurality of surface curves, a selected data point of the plurality of data points on the selected surface curve, and a selected rotation angle. The method further includes determining an output dimension, location, and orientation of a passive strain indicator. The method further includes providing one or more control signals to a passive strain indicator application system to cause the system to apply the passive strain indicator having the output dimension, location, and orientation to the component.

Abstract: A computer-implemented method for applying passive strain indicators to a component includes creating a plurality of surface curves and a plurality of data points on each of the plurality of surface curves, the plurality of surface curves and the plurality of data points defining the exterior surface of the component. The method further includes receiving data indicative of a user input selection of a selected surface curve of the plurality of surface curves, a selected data point of the plurality of data points on the selected surface curve, and a selected rotation angle. The method further includes determining an output dimension, location, and orientation of a passive strain indicator. The method further includes providing one or more control signals to a passive strain indicator application system to cause the system to apply the passive strain indicator having the output dimension, location, and orientation to the component.

Abstract: A computer-implemented method for applying passive strain indicators to a component includes obtaining an output dimension, location, and orientation of each of a plurality of passive strain indicators for the component. The method further includes determining an inverse rotation matrix for each of the plurality of passive strain indicators based on the orientation and location of each of the plurality of passive strain indicators. The method further includes determining a movement profile for each of the plurality of passive strain indicators based on the inverse rotation matrix. The method further includes providing one or more control signals to a passive strain indicator application system to cause the system to apply each of the plurality of passive strain indicators to the component based on the movement profile for each of the plurality of passive strain indicators.