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发表于 2006-7-21 07:42:48
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机翼涡流冲量理论
下面引用由nasalaoliu在 2006/07/11 04:16am 发表的内容:
感谢李博士的到来,希望各位高手互相转告多多捧场,这是一个和李博士交流的好机会,李博士对空气动力学理论所作的贡献值得所有中国人称赞.希望大家尤其高手抽出时间来共同讨论这个理论.谢谢大家! Thank you Lao Liu,
Please also look at my second paper "李湘渝的新論文" where the computations are compared to experimental results.
If you are famliar with the "Leading Edge Suction Analogy" approach (Polhamus,AIAA, J. Aircraft 1971, Lamar, NASA TR R-428, 1974, etc) you will find that their theory for non-linear lift is totally ridiculous.But that theory has been popular for many years in Western circles. In my scond paper, I have proposed a representation of non-linear lift. And together with the linear theory, they provide very good match to experiments in all cases.
The theory can be verified by experiments or computational methods, provided the computation model is correctly formulated. If some of you are good at that, I hope you can verify my observations of how reactive flows should be distributed around the wing. |
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