Investigation of creep life optimization of a high-pressure turbine rotor blade with ribbed internal cooling channels
Author:
Dehai Kong,Xueying Tian,Xuemin Lv,Wenbin Chen,Yihong He,Junxing Tang,Sergey Isaev,Cunliang Liu
Publication:
Aerospace Science and Technology
Date:
Available online 13 June 2026
© 2026 Elsevier Masson SAS. All rights are reserved, including those for text and data mining, AI training, and similar technologies.