- 期刊
Heat Transfer Augmentation Technologies for Internal Cooling of Turbine Components of Gas Turbine Engines
被引用紀錄
蘭宜安（2019）。旋轉平行四邊形急彎雙肋化通道熱傳性能實驗研究〔博士論文，國立清華大學〕。華藝線上圖書館。https://www.airitilibrary.com/Article/Detail?DocID=U0016-0206202016125385
延伸閱讀
- 李信龍（2014）。A Study of Heat Transfer for Internal Cooling Passage of Gas Turbine Blades〔博士論文，國立清華大學〕。華藝線上圖書館。https://www.airitilibrary.com/Article/Detail?DocID=U0016-2912201413503479
- AYDIN, O., IWATA, M., ARAI, N., & YANG, W. J. (2002). Theoretical Analysis of Heat Transfer Through an Idealized Gas Turbine Blade Model with Thermal Barrier Coating. International Journal of Rotating Machinery, 2002(), 81-86. https://doi.org/10.1155/S1023621X02000088
- 黃建勝（2004）。A Study of Heat Transfer for Impingement Cooling on Hot Spot of Electronic Components〔碩士論文，中原大學〕。華藝線上圖書館。https://doi.org/10.6840/cycu200400359
- Batsh, H. M. E., Nada, S. A., Abdo, S. N., & Tayesh, A. A. E. (2013). Effect of Secondary Flows on Heat Transfer of a Gas Turbine Blade. International Journal of Rotating Machinery, 2013(), 179-190. https://doi.org/10.1155/2013/797841
- 黎沛伶、鄭敦仁、柯皇卲、高騏（2010）。Fabrication and Performance Evaluation of a Micro Film-Cooled Device for Gas Turbine Blade Cooling Effectiveness。航空太空及民航學刊.系列B，42(1)，37-41。https://doi.org/10.6124/JAAA.201004_42(1).05