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- Author: Jamie J Johnson
- Publisher: BiblioScholar
- ISBN-10: 124959510X
- ISBN-13: 9781249595106
- Format: 18.9 x 24.6 x 1.2 cm, minkšti viršeliai
- Language: English
- SAVE -10% with code: EXTRA
Optimization of a Low Heat Load Turbine Nozzle Guide Vane (e-book) (used book) | bookbook.eu
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Description
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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- Author: Jamie J Johnson
- Publisher: BiblioScholar
- ISBN-10: 124959510X
- ISBN-13: 9781249595106
- Format: 18.9 x 24.6 x 1.2 cm, minkšti viršeliai
- Language: English English
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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