City Research Online

Items where Author is "He, L."

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Rondao, D. ORCID: 0000-0001-9438-0267, He, L. ORCID: 0000-0003-3028-6305 & Aouf, N. ORCID: 0000-0001-9291-4077 (2024). AI-based monocular pose estimation for autonomous space refuelling. Acta Astronautica, doi: 10.1016/j.actaastro.2024.04.003

Jiang, H., He, L., Zhang, Q. & Wang, L. (2018). On scaling method to investigate high-speed over-tip-leakage flow at low-speed condition. Journal of Engineering for Gas Turbines and Power, 140(6), article number 062605. doi: 10.1115/1.4038619

Jiang, H., Chen, W., Zhang, Q. & He, L. (2015). Analytical-Solution Based Corner Correction for Transient Thermal Measurement. Journal of Heat Transfer, 137(11), article number 111302. doi: 10.1115/1.4030980

Wang, Z., Zhang, Q., Liu, Y. & He, L. (2015). Impact of Cooling Injection on the Transonic Over-Tip Leakage Flow and Squealer Aerothermal Design Optimization. Journal of Engineering for Gas Turbines and Power, 137(6), article number 062603. doi: 10.1115/1.4029120

Virdi, A. S., Zhang, Q., He, L. , Li, H. D. & Hunsleys, R. (2015). Aerothermal Performance of Shroudless Turbine Blade Tips with Relative Casing Movement Effects. Journal of Propulsion and Power, 31(2), pp. 527-536. doi: 10.2514/1.b35331

Zhang, Q. & He, L. (2014). Impact of wall temperature on turbine blade tip aerothermal performance. Journal of Engineering for Gas Turbines and Power, 136(5), article number 52602. doi: 10.1115/1.4026001

Zhang, Q. & He, L. (2013). Tip-shaping for HP turbine blade aerothermal performance management. Journal of Turbomachinery, 135(5), doi: 10.1115/1.4007896

Zhang, Q., D'Dowd, D., Wheeler, A. P. S. , He, L., Ligrani, P. & Cheong, B. C. Y. (2011). Over-tip shock wave structure and its impact on turbine blade heat transfer. Journal of Turbomachinery, 133(4), article number 41001. doi: 10.1115/1.4002949

Zhang, Q. & He, L. (2011). Over-Tip Choking and Its Implications on Turbine Blade Tip Aerodynamic Performance. Journal of Propulsion and Power, 27(5), pp. 1008-1014. doi: 10.2514/1.b34112

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