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Solution of Falkner—Skan Equations for Hypersonic Flows
Fluid Dynamics ( IF 1.0 ) Pub Date : 2020-07-01 , DOI: 10.1134/s0015462820040072
I. I. Lipatov , K. T. Ngo

The results of the solution of the Falkner—Skan equation for compressible flows $$f{\kern 1pt} ''' + ff{\kern 1pt} '' + \beta (g - f{{'}^{2}}) = 0$$ are obtained for the first time, in addition to those obtained by Hartree and Stewartson. The dependence of the viscous stress $$f_{w}^{{''}}$$ at the wall and the temperature gradient $$g_{w}^{'}$$ on the parameter $$\beta $$ is determined for different values of the temperature factor gw.

中文翻译:

Falkner 的解——高超声速流动的 Skan 方程

可压缩流的 Falkner-Skan 方程的求解结果 $$f{\kern 1pt} ''' + ff{\kern 1pt} '' + \beta (g - f{{'}^{2}} ) = 0$$ 是第一次获得,除了 Hartree 和 Stewartson 获得的那些。壁面粘性应力 $$f_{w}^{{''}}$$ 和温度梯度 $$g_{w}^{'}$$ 对参数 $$\beta $$ 的依赖性为为不同的温度因子 gw 值确定。
更新日期:2020-07-01
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