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牛顿流理论及其在谐振机翼上的应用
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作者 陈劲松 《空气动力学学报》 CSCD 北大核心 1993年第2期232-238,共7页
根据牛顿流理论,文中讨论了高马赫数、任意迎角、一般剖面在均匀来流中作沉浮和俯仰谐振的翼型和机翼。导得翼型和机翼表面的牛顿撞击压强和安定性导数公式。给出楔、平板三角翼、双抛物线剖面三角翼俯仰刚性导数(-C_(mθ)和阻尼导数(-C... 根据牛顿流理论,文中讨论了高马赫数、任意迎角、一般剖面在均匀来流中作沉浮和俯仰谐振的翼型和机翼。导得翼型和机翼表面的牛顿撞击压强和安定性导数公式。给出楔、平板三角翼、双抛物线剖面三角翼俯仰刚性导数(-C_(mθ)和阻尼导数(-C_(m))的数值例子。数值结果与现有的牛顿-布兹曼流理论、薄激波层理论、欧拉方程摄动理论的结果作了比较,算例表明本文的结果令人满意。 展开更多
关键词 非定常 牛顿流理论 机翼
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球锥表面压力分布和静态气动力特性的工程计算方法
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作者 周其成 《中国空间科学技术》 EI 1984年第5期1-16,23,共17页
本文沿用内伏牛顿流基本思想,改进爆炸波理论在钝头附近的逼近精度,利用球锥无粘流数值解的零攻角表面压力数据(M_∞=4~8,θ_c=2.5°~20°)和轴对称比拟方法,拟合了一套既适用于短钝锥,又适合于细长锥的气动力工程方法。计算... 本文沿用内伏牛顿流基本思想,改进爆炸波理论在钝头附近的逼近精度,利用球锥无粘流数值解的零攻角表面压力数据(M_∞=4~8,θ_c=2.5°~20°)和轴对称比拟方法,拟合了一套既适用于短钝锥,又适合于细长锥的气动力工程方法。计算表明,本文提出的拟合公式计算精度优于Ericsson的内伏牛顿流理论和Blick的分段公式的精度,球锥几倍头部半径范围之内零攻角和有攻角表面压力分布计算误差分别为5%和10%左右,在稍远的地方逼近内伏牛顿流理论;气动力系数(C_A、C_N、C_M和X_(CP)/L)的计算值与数值解和风洞测力试验的测量结果吻合良好。 展开更多
关键词 牛顿流理论 攻角 表面压力 数值解 迎角 数值分析 球锥 气动力系数 钝锥 压力分布 分布(力学)
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Introduction to the Turbulent Flows Theory--An Axially-Symmetric Non-peaceful Flows
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作者 Tomasz M. Jankowski 《Journal of Mechanics Engineering and Automation》 2014年第4期327-357,共31页
In fluid mechanics, there is lack of turbulent flows theory. The theory of laminar flows is also not completed. Therefore, the aim of this paper is to fill in the gaps in the theory of laminar flow. First time in the ... In fluid mechanics, there is lack of turbulent flows theory. The theory of laminar flows is also not completed. Therefore, the aim of this paper is to fill in the gaps in the theory of laminar flow. First time in the history of fluid mechanics, it shows that the value of the boundary Reynolds number, dividing the flows of Newtonian fluids into laminar and turbulent, can be calculated theoretically. The very existence of this boundary has been known to researchers over a century ago, but all knowledge in this area so far comes only from experimental physics. This paper marks a turning point, as it not only explains the theory of the said phenomenon, but also presents the methodology of its analytical description. It should be noted that the said description refers to the type of flow which is best understood by scientists, i.e., steady axially-symmetric laminar flow through a straight-axis duct of a circular cross-section of the radius R under the action of constant natural gravitational forces. This paper comes second in a series of papers aimed at eliminating chaos from fluid mechanics and replacing it with harmony and mathematical order. 展开更多
关键词 Dualism theory primary motion secondary motion.
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