Abstract
Introduction. The problem of POD of NDT is very important for Russian aerospace industry nowadays. Using FAAACС 33.14 data is inexpedient because of significant difference between Russian and foreign titanium disks ultrasonic testing NDT manuals. Probability of defect detection versus its size curves are necessary for the deficiency evaluation of gas-turbine engine basic parts. Evaluation of gas-turbine engine basic parts deficiency is necessary for new procedure of resource calculation introduction.
Sign-in/Register to access full text options 
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a callDisclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.
