TY  - CONF

T1  - Multidisciplinary Optimisation of High Pressure Turbine Blade Tip With Turbine Inlet Capacity and Stage Reaction Constraints

JO  - AIAA AVIATION 2021 FORUM

PY  - 2021/07/28

AU  - Vincekovic L

AU  - Qin N

AU  - Shahpar S

ED  - 

DO  - DOI: 10.2514/6.2021-3071

PB  - American Institute of Aeronautics and Astronautics

Y2  - 2024/12/27

ER  -