Aerofoil profile and sweep optimisation for a blended wing-body aircraft using a discrete adjoint method

被引：0
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作者：
Le Moigne, A. [1 ]
Qln, N. [1 ]
机构：
[1] Department of Mechanical Engineering, University of Sheffield, Sheffield, United Kingdom
来源：
Aeronautical Journal | 2006年 / 110卷 / 1111期
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页码：589 / 604
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