Unsteady Adjoint of Pressure Loss for a Fundamental Transonic Turbine Vane
High fidelity simulations, e.g., large eddy simulation are often needed for accurately predicting pressure losses due to wake mixing and boundary layer development in turbomachinery applications. An unsteady adjoint of high fidelity simulations is useful for design optimization in such aerodynamic a...
Main Authors: | Laskowski, Gregory M. (Author), Talnikar, Chaitanya Anil (Contributor), Wang, Qiqi (Contributor) |
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Other Authors: | Massachusetts Institute of Technology. Department of Aeronautics and Astronautics (Contributor), Massachusetts Institute of Technology. Computation for Design and Optimization Program (Contributor) |
Format: | Article |
Language: | English |
Published: |
ASME International,
2018-06-11T16:02:14Z.
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Subjects: | |
Online Access: | Get fulltext |
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