Steady and unsteady pressure measurements on a swept-wing aircraft

被引：0
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作者：
机构：
[1] Jansson, N.
[2] Stenfelt, G.
来源：
| 1600年 / Royal Aeronautical Society卷 / 118期
关键词：
Reynolds number - Computation theory - Swept wings;
D O I：
10.1017/S0001924000009015
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