Aerodynamic design of transsonic compressor airfoil family

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F21%3A00357234" target="_blank" >RIV/68407700:21220/21:00357234 - isvavai.cz</a>
Result on the web
<a href="https://www.kme.zcu.cz/compmech/download/proceedings/CM2021_Conference_Proceedings.pdf" target="_blank" >https://www.kme.zcu.cz/compmech/download/proceedings/CM2021_Conference_Proceedings.pdf</a>
DOI - Digital Object Identifier
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Result language
angličtina
Original language name
Aerodynamic design of transsonic compressor airfoil family
Original language description
New family of transsonic compressor airfoils is being developed in the frame of KOBRA project. This project is focused on the development of new gas-cooled nuclear reactor and axial compressor is a part of the secondary system. Maximum Mach number based on intake velocity is assumed 0.8, which gives compromise between high stage pressure ratio and low loss coefficient. New airfoil family should have better performance that classical NACA 65 airfoils, but it should offer performance comparable with the Controlled Diffusion Airfoils (CDA).
Czech name
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Czech description
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Project
<a href="/en/project/TK03030121" target="_blank" >TK03030121: Conceptual Design of an Innovative Safety System for Gas-cooled Nuclear Reactors</a><br>
Continuities
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Publication year
2021
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

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