Date of download: 10/6/2017 Copyright © ASME. All rights reserved. From: The Influence of Friction Stir Welding Process Idealization on Residual Stress and Distortion Predictions for Future Airframe Assembly Simulations J. Manuf. Sci. Eng. 2012;134(3):031011-031011-9. doi:10.1115/1.4006554 Figure Legend: A typical fuselage stiffened panel assembly
Date of download: 10/6/2017 Copyright © ASME. All rights reserved. From: The Influence of Friction Stir Welding Process Idealization on Residual Stress and Distortion Predictions for Future Airframe Assembly Simulations J. Manuf. Sci. Eng. 2012;134(3):031011-031011-9. doi:10.1115/1.4006554 Figure Legend: Schematic of friction stir welding process
Date of download: 10/6/2017 Copyright © ASME. All rights reserved. From: The Influence of Friction Stir Welding Process Idealization on Residual Stress and Distortion Predictions for Future Airframe Assembly Simulations J. Manuf. Sci. Eng. 2012;134(3):031011-031011-9. doi:10.1115/1.4006554 Figure Legend: Schematic of future airframe manufacturing philosophy
Date of download: 10/6/2017 Copyright © ASME. All rights reserved. From: The Influence of Friction Stir Welding Process Idealization on Residual Stress and Distortion Predictions for Future Airframe Assembly Simulations J. Manuf. Sci. Eng. 2012;134(3):031011-031011-9. doi:10.1115/1.4006554 Figure Legend: Validation component plus refined FE mesh
Date of download: 10/6/2017 Copyright © ASME. All rights reserved. From: The Influence of Friction Stir Welding Process Idealization on Residual Stress and Distortion Predictions for Future Airframe Assembly Simulations J. Manuf. Sci. Eng. 2012;134(3):031011-031011-9. doi:10.1115/1.4006554 Figure Legend: Time history of torque and forging force before and during welding process
Date of download: 10/6/2017 Copyright © ASME. All rights reserved. From: The Influence of Friction Stir Welding Process Idealization on Residual Stress and Distortion Predictions for Future Airframe Assembly Simulations J. Manuf. Sci. Eng. 2012;134(3):031011-031011-9. doi:10.1115/1.4006554 Figure Legend: Simulation and experimentally measured temperature history
Date of download: 10/6/2017 Copyright © ASME. All rights reserved. From: The Influence of Friction Stir Welding Process Idealization on Residual Stress and Distortion Predictions for Future Airframe Assembly Simulations J. Manuf. Sci. Eng. 2012;134(3):031011-031011-9. doi:10.1115/1.4006554 Figure Legend: Validation component tool surface out-of-plane distortions—lateral planes
Date of download: 10/6/2017 Copyright © ASME. All rights reserved. From: The Influence of Friction Stir Welding Process Idealization on Residual Stress and Distortion Predictions for Future Airframe Assembly Simulations J. Manuf. Sci. Eng. 2012;134(3):031011-031011-9. doi:10.1115/1.4006554 Figure Legend: Validation component tool surface out-of-plane distortions—longitudinal planes
Date of download: 10/6/2017 Copyright © ASME. All rights reserved. From: The Influence of Friction Stir Welding Process Idealization on Residual Stress and Distortion Predictions for Future Airframe Assembly Simulations J. Manuf. Sci. Eng. 2012;134(3):031011-031011-9. doi:10.1115/1.4006554 Figure Legend: Predicted and measured longitudinal residual stress
Date of download: 10/6/2017 Copyright © ASME. All rights reserved. From: The Influence of Friction Stir Welding Process Idealization on Residual Stress and Distortion Predictions for Future Airframe Assembly Simulations J. Manuf. Sci. Eng. 2012;134(3):031011-031011-9. doi:10.1115/1.4006554 Figure Legend: Dominant process modeling effects
Date of download: 10/6/2017 Copyright © ASME. All rights reserved. From: The Influence of Friction Stir Welding Process Idealization on Residual Stress and Distortion Predictions for Future Airframe Assembly Simulations J. Manuf. Sci. Eng. 2012;134(3):031011-031011-9. doi:10.1115/1.4006554 Figure Legend: Interaction of modeling effects
Date of download: 10/6/2017 Copyright © ASME. All rights reserved. From: The Influence of Friction Stir Welding Process Idealization on Residual Stress and Distortion Predictions for Future Airframe Assembly Simulations J. Manuf. Sci. Eng. 2012;134(3):031011-031011-9. doi:10.1115/1.4006554 Figure Legend: Longitudinal residual stresses with and without torque