Examination and Prediction of the Lift Components of Low Aspect Ratio Rectangular Flat Plate Wings
An investigation of the lift components present over low aspect ratio rectangular wings is presented. Wing aspect ratios ranging from 0.5 to 3 are examined using published experimental results and analytic analysis methods. The methods are based on the fundamental decomposition of Polhamus; that is,...
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| Format: | Article |
| Language: | English |
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MDPI AG
2023-06-01
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| Series: | Aerospace |
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| Online Access: | https://www.mdpi.com/2226-4310/10/7/597 |