@inproceedings{inproceedings, title  = {{Multidisciplinary Optimisation of High Pressure Turbine Blade Tip With Turbine Inlet Capacity and Stage Reaction Constraints}},

 publisher = {{American Institute of Aeronautics and Astronautics}},

 url = {{https://doi.org/10.2514/6.2021-3071 }},

 year = {{2021}},

 month = {{7}},

 author = {{Vincekovic L and Qin N and Shahpar S}},

 doi = {{10.2514/6.2021-3071}},

 journal = {{AIAA AVIATION 2021 FORUM}},

 note = {{Accessed on 2025/11/03}}}