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- W2029402699 abstract "A brief description is given of the outboard-horizontal-stabilizer concept and relevant background material. Wind-tunnel tests were conducted to investigate the influence of main-plane aspect ratio on the flowfields prevailing in the vicinity of the tail surfaces located essentially downwind of the wing tips. It was found that variation of aspect ratio had, for a prescribed wing lift coefficient, substantially zero influence on the flow pattern. Partly as a consequence of this finding, simple equations were derived describing the flowfields interacting with the tail surfaces. These analytical results were employed in predicting the performance of optimized outboard horizontal stabilizer aircraft covering a range of aspect ratios from 6 to 15.It was concluded that these aircraft had cruise drag values between 20 and 45% less, with planform areas typically 15% lower, than those of comparable conventional aircraft" @default.
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- W2029402699 date "2000-01-01" @default.
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- W2029402699 title "Influence of Aspect Ratio on the Performance of Outboard-Horizontal-Stabilizer Aircraft" @default.
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- W2029402699 doi "https://doi.org/10.2514/2.2562" @default.
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