Numerical analysis and experimental study on aerodynamic shape of support structure considering wind tunnel flow quality
Aircraft continuously change their flight attitudes during actual operations. If a constant attitude is maintained during wind tunnel tests, the aerodynamic characteristics obtained may significantly deviate from the actual performance of the aircraft. Such discrepancies hinder the optimal design of...
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| Main Authors: | , , , , , , |
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| Format: | Article |
| Language: | English |
| Published: |
SAGE Publishing
2025-06-01
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| Series: | Advances in Mechanical Engineering |
| Online Access: | https://doi.org/10.1177/16878132251348284 |
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