𝗔𝗦𝗠𝗘 𝗧𝘂𝗿𝗯𝗼 𝗘𝘅𝗽𝗼 𝟮𝟬𝟮𝟱

Looking back at 𝗔𝗦𝗠𝗘 𝗧𝘂𝗿𝗯𝗼 𝗘𝘅𝗽𝗼 𝟮𝟬𝟮𝟱, we want to highlight Morfo’s contribution to the discussion on future turbine technologies.
Together with our partners from universities and industry, we presented three works addressing different aspects of low-pressure turbine aerodynamics:

🔹 𝗧𝗶𝗽 𝗹𝗲𝗮𝗸𝗮𝗴𝗲 𝗳𝗹𝗼𝘄𝘀 𝗶𝗻 𝘀𝗾𝘂𝗲𝗮𝗹𝗲𝗿 𝗟𝗣𝗧 𝗯𝗹𝗮𝗱𝗲𝘀 — combining experiments and 3D-RANS to analyze how clearance and coolant ejection affect secondary vortices.
“𝘕𝘶𝘮𝘦𝘳𝘪𝘤𝘢𝘭 𝘈𝘯𝘥 𝘌𝘹𝘱𝘦𝘳𝘪𝘮𝘦𝘯𝘵𝘢𝘭 𝘈𝘯𝘢𝘭𝘺𝘴𝘪𝘴 𝘖𝘧 𝘛𝘩𝘦 𝘛𝘪𝘱 𝘓𝘦𝘢𝘬𝘢𝘨𝘦 𝘍𝘭𝘰𝘸 𝘐𝘯 𝘈 𝘚𝘲𝘶𝘦𝘢𝘭𝘦𝘳 𝘓𝘗𝘛 𝘉𝘭𝘢𝘥𝘦 𝘍𝘰𝘳 𝘋𝘪𝘧𝘧𝘦𝘳𝘦𝘯𝘵 𝘖𝘱𝘦𝘳𝘢𝘵𝘪𝘯𝘨 𝘊𝘰𝘯𝘥𝘪𝘵𝘪𝘰𝘯𝘴”

🔹 𝗘𝗻𝗱𝘄𝗮𝗹𝗹 𝗿𝗶𝗱𝗴𝗶𝗻𝗴 𝗼𝗽𝘁𝗶𝗺𝗶𝘇𝗮𝘁𝗶𝗼𝗻 — parametric CFD design and experimental validation to mitigate passage vortex effects and enhance performance of an aggressive NGV.
“𝘖𝘱𝘵𝘪𝘮𝘪𝘻𝘢𝘵𝘪𝘰𝘯 𝘖𝘧 𝘌𝘯𝘥𝘸𝘢𝘭𝘭 𝘙𝘪𝘥𝘨𝘪𝘯𝘨 𝘍𝘰𝘳 𝘌𝘯𝘩𝘢𝘯𝘤𝘦𝘥 𝘌𝘧𝘧𝘪𝘤𝘪𝘦𝘯𝘤𝘺 𝘐𝘯 𝘈𝘨𝘨𝘳𝘦𝘴𝘴𝘪𝘷𝘦 𝘛𝘶𝘳𝘣𝘪𝘯𝘦 𝘝𝘢𝘯𝘦𝘥 𝘋𝘶𝘤𝘵𝘴”

🔹 𝗧𝗮𝗶𝗹𝗯𝗼𝗮𝗿𝗱 𝗰𝗼𝗻𝗳𝗶𝗴𝘂𝗿𝗮𝘁𝗶𝗼𝗻 𝗶𝗻 𝘁𝗿𝗮𝗻𝘀𝗼𝗻𝗶𝗰 𝗟𝗣𝗧 𝗰𝗮𝘀𝗰𝗮𝗱𝗲𝘀 — investigating how different tailboard geometries influence periodicity and aerodynamic behavior at Mach 0.8–1.2.
“𝘐𝘮𝘱𝘢𝘤𝘵 𝘖𝘧 𝘛𝘢𝘪𝘭𝘣𝘰𝘢𝘳𝘥 𝘊𝘰𝘯𝘧𝘪𝘨𝘶𝘳𝘢𝘵𝘪𝘰𝘯 𝘖𝘯 𝘍𝘭𝘰𝘸 𝘗𝘦𝘳𝘪𝘰𝘥𝘪𝘤𝘪𝘵𝘺 𝘐𝘯 𝘛𝘳𝘢𝘯𝘴𝘰𝘯𝘪𝘤 𝘓𝘰𝘸-𝘗𝘳𝘦𝘴𝘴𝘶𝘳𝘦 𝘛𝘶𝘳𝘣𝘪𝘯𝘦 𝘊𝘢𝘴𝘤𝘢𝘥𝘦𝘴”
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Beyond the technical results, Turbo Expo was once again a valuable reminder of how much progress is achieved through collaboration and knowledge sharing.
It was an opportunity to reconnect with colleagues and friends worldwide, and to engage with the work of the most relevant research centers, universities, and industries in the field.
At Morfo, we are proud to contribute to this collective effort: advancing the design of ever more efficient machines and shaping the technologies of tomorrow.