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Opis

Often turbomachinery airfoils are designed with aerodynamic performance foremost in mind rather than component durability. However, future aircraft systems require ever increasing levels of gas-turbine inlet temperature causing the durability and reliability of turbine components to be an ever more important design concern. As a result, the need to provide improved heat transfer prediction and optimization methods presents itself. Here, an effort to design an airfoil with minimized heat load is reported. First, a Reynolds-Averaged Navier-Stokes (RANS) flow solver was validated over different flow regimes as well as varying boundary conditions against extensive data available in literature published by the Von Karman Institute (VKI).

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Kategoria Książki po angielsku Society & social sciences Education

• Pełny tytuł: Optimization of a Low Heat Load Turbine Nozzle Guide Vane
• Autor: Jamie J Johnson
• Język: Angielski
• Oprawa: Miękka
• Liczba stron: 222
• EAN: 9781249595106
• ISBN: 9781249595106
• ID: 08142506
• Wydawca: Biblioscholar
• Waga: 404 g
• Wymiary: 246 × 189 × 12 mm
• Data wydania: 09. October 2012

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