Optimal shape design using an unsteady continuous adjoint approach
Many practical flows of aerodynamic interest are unsteady in nature, and between increases in computing power and advanced algorithms, accurately predicting and designing for the performance of aerospace systems in an unsteady environment is becoming more tractable. Several examples of engineering a...
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| Format: | Thesis Electronic Book |
| Language: | English |
| Published: |
2014
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Internet
This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.Stanford University
| Call Number: |
3781 2014 E INTERNET RESOURCE |
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