Numerical investigation of high pressure turbine blade tip-shaping effects on the aerothermal and dynamic performance | Emerald Insight
![A review of blade tip clearance–measuring technologies for gas turbine engines - Bing Yu, Hongwei Ke, Enyu Shen, Tianhong Zhang, 2020 A review of blade tip clearance–measuring technologies for gas turbine engines - Bing Yu, Hongwei Ke, Enyu Shen, Tianhong Zhang, 2020](https://journals.sagepub.com/cms/10.1177/0020294019877514/asset/images/large/10.1177_0020294019877514-fig7.jpeg)
A review of blade tip clearance–measuring technologies for gas turbine engines - Bing Yu, Hongwei Ke, Enyu Shen, Tianhong Zhang, 2020
![Influences of a multi-cavity tip on the blade tip and the over tip casing aerothermal performance in a high pressure turbine cascade - ScienceDirect Influences of a multi-cavity tip on the blade tip and the over tip casing aerothermal performance in a high pressure turbine cascade - ScienceDirect](https://ars.els-cdn.com/content/image/1-s2.0-S1359431118347495-gr5.jpg)
Influences of a multi-cavity tip on the blade tip and the over tip casing aerothermal performance in a high pressure turbine cascade - ScienceDirect
![A review of blade tip clearance–measuring technologies for gas turbine engines - Bing Yu, Hongwei Ke, Enyu Shen, Tianhong Zhang, 2020 A review of blade tip clearance–measuring technologies for gas turbine engines - Bing Yu, Hongwei Ke, Enyu Shen, Tianhong Zhang, 2020](https://journals.sagepub.com/cms/10.1177/0020294019877514/asset/images/large/10.1177_0020294019877514-fig3.jpeg)
A review of blade tip clearance–measuring technologies for gas turbine engines - Bing Yu, Hongwei Ke, Enyu Shen, Tianhong Zhang, 2020
![Figure 2 from Assessment of various rotor tip geometries on a single stage gas turbine performance | Semantic Scholar Figure 2 from Assessment of various rotor tip geometries on a single stage gas turbine performance | Semantic Scholar](https://d3i71xaburhd42.cloudfront.net/704371a277bfb2d9f9f68de67e4eba7e07869054/6-Figure2-1.png)