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Wind tunnel support system effects on a fighter aircraft model at Mach numbers from 0.6 to 2.0
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已完结
Correction of support influences on measurements with sting mounted wind tunnel models
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Model support system interference on zero-lift drag at transonic speeds
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CFD support to wind tunnel experiments
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The crucial role of wall interference, support interference and flow field measurements in the development of advanced aircraft configurations
4个月前
已关闭
Wind tunnel support system effects on a fighter aircraft model at Mach numbers from 0.6 to 2.0
4个月前
已完结
Wind-tunnel experiments on divergence of forward-swept wings
9个月前
已完结
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