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).
General
| Imprint: |
Biblioscholar
|
| Country of origin: |
United States |
| Release date: |
October 2012 |
| First published: |
October 2012 |
| Authors: |
Jamie J Johnson
|
| Dimensions: |
246 x 189 x 12mm (L x W x T) |
| Format: |
Paperback - Trade
|
| Pages: |
222 |
| ISBN-13: |
978-1-249-59510-6 |
| Categories: |
Books >
Social sciences >
Education >
General
|
| LSN: |
1-249-59510-X |
| Barcode: |
9781249595106 |
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