Numerical Study of Attack Angle Characteristics for Integrated Hypersonic Vehicle
一体化高超声速飞行器攻角特性的数值研究
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Optimum design and analysis of a centrifugal compressor with large attack angle
大攻角离心压气机优化设计与分析
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Application of Quantitative Feedback Theory to Attack Angle Robust Control System of Missile
数量反馈理论在导弹攻角鲁棒控制系统中的应用
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Influence of Attack Angle and Lateral Force on the wheel Flange wear of Locomotive
冲角和横向力对机车轮缘磨损的影响
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The Design for Autopilot of Large Attack Angle Missile by Using Feedback Linearization Method
大攻角飞行导弹自动驾驶仪反馈线性化设计
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首先建立了高超声速导弹再入段弹道模型,并将攻角作为控制变量。
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结果表明:涂层的冲蚀磨损受到攻角、冲速、磨料量等多种因素的影响。
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一维弹道修正引信阻力器空气阻力的简捷测量,是在弹丸零攻角、低风速下测量空气阻力的试验方法。
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本方法可用于计算来流马赫数为0到3.5左右、攻角和侧滑角为0°到20°左右、正常式或鸭式布局的战术弹纵、横向气动力系数。
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The angle of attack of the high-aspect-ratio wings varies largely as the airflow rounds the airfoil.
在飞行状态下气流绕过翼型时,大展弦比机翼的迎角变化范围非常大.
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The velocity distributions previously shown were for a single angle of attack.
先前的速度分布列分别为单一迎角.
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The static aerodynamic characteristics for slender bodies at large angle of attack was analyzed.
研究分析了细长旋成体弹身类型气动外形的大攻角范围气动特性.
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The measurement of the model angle of attack is a key part in wind tunnel test.
模型迎角的测量是风洞试验中非常重要的环节.
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