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AbstractTo support the design of a two-dimensional turbine blade profile with reduced shock loss, an efficient model for shock system with separation shock in highly loaded turbine cascade needed t... Click to show full abstract
AbstractTo support the design of a two-dimensional turbine blade profile with reduced shock loss, an efficient model for shock system with separation shock in highly loaded turbine cascade needed t...
Keywords:
turbine;
shock system;
turbine cascade;
highly loaded;
loaded turbine;
shock
Journal Title: Journal of Aerospace Engineering
Year Published: 2020
Link to full text (if available)
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Journal Title: Journal of Aerospace Engineering
Year Published: 2020
Link to full text (if available)
Share on Social Media: Sign Up to like & get
recommendations!