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(Created page with "Purpose: 1. Identify and lay out a roadmap for the implementation of engineered deep residual stress which can be used in the calculation of initial and recurring inspection intervals for fatigue and fracture critical aerospace components. 2. Highlight gaps in the state-of-the-art and define how those gaps will be filled. 3. Define the most effective way to document requirements and guidelines for fleet-wide implementation. Working Group Structure: Committee:Residual...")
 
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Purpose:
Purpose:
1. Identify and lay out a roadmap for the implementation of
1. Identify and lay out a roadmap for the implementation of engineered deep residual stress which can be used in the calculation of initial and recurring inspection intervals for fatigue and fracture critical aerospace components. <br>
engineered deep residual stress which can be used in the
2. Highlight gaps in the state-of-the-art and define how those gaps will be filled. <br>
calculation of initial and recurring inspection intervals for fatigue
3. Define the most effective way to document requirements and guidelines for fleet-wide implementation.
and fracture critical aerospace components.
2. Highlight gaps in the state-of-the-art and define how those gaps
will be filled.
3. Define the most effective way to document requirements and
guidelines for fleet-wide implementation.


Working Group Structure:
Working Group Structure:
[[Committee:Residual Stress Process Simulation]]
[[Committee:Residual Stress Process Simulation]]
[[Committee:Verification and Validation Testing]]
[[Committee:Verification and Validation Testing]]

Revision as of 21:48, 5 December 2022

Purpose: 1. Identify and lay out a roadmap for the implementation of engineered deep residual stress which can be used in the calculation of initial and recurring inspection intervals for fatigue and fracture critical aerospace components.
2. Highlight gaps in the state-of-the-art and define how those gaps will be filled.
3. Define the most effective way to document requirements and guidelines for fleet-wide implementation.

Working Group Structure: Committee:Residual Stress Process Simulation Committee:Verification and Validation Testing