Positive Tail Loads for Minimum Induced Drag of Subsonic Aircraft
By applying Prandtl's relation for the induced drag of a biplane to typical wing-tail combinations, it can be shown that the minimum induced drag occurs with a positive tail upload. This fact has been overlooked because the reduction in the total induced drag by a tail download was overestimate...
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| Veröffentlicht in: | Journal of aircraft 1978-12, Vol.15 (12), p.837-842 |
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| Format: | Artikel |
| Sprache: | eng |
| Online-Zugang: | Volltext |
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