Abstract
항공기 가스터빈 엔진 위험도 평가 사례 연구: 아크 바인딩에 의한 CT7 엔진 1단계 터빈 블레이드 피로 균열
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
More From: Transactions of the Korean Society of Mechanical Engineers - A
Disclaimer: 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.