The recent progress in the design of structural strength and life assessment for aero-engine single crystal turbine blades
Author:
Affiliation:
1. State Key Laboratory of Efficient and Clean Turbomachinery Power Equipment, Northwestern Polytechnical University, PR China
Funder
National Natural Science Foundation of China
Publisher
Informa UK Limited
Link
https://www.tandfonline.com/doi/pdf/10.1080/09603409.2024.2325214
Reference45 articles.
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3. MacIsaac B, Langton R, Belobaba P, et al. Gas turbine propulsion systems. John Wiley & Sons; 2011.
4. Precise infrared thermometry with considering background radiation for gas turbine air cooling application
5. Effect of turbine inlet temperature on rotor blade tip leakage flow and heat transfer
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