15th Asian Congress of Fluid Mechanics | |
Analytical solution of subsonic gas flow past a circle | |
物理学;力学 | |
Mansour, Kamyar^1,2 | |
Department of Aerospace Engineering, AmirKabir University of Technology, Tehran | |
1587-4413, Iran^1 | |
Flow Research and Engineering, 788 Maplewood Avenue, Palo Alto | |
CA | |
94303, Iran^2 | |
关键词: Diatomic gas; Maximum velocity; Potential function; Radius of convergence; Series expansion; Two-dimension; Two-dimensional flow; | |
Others : https://iopscience.iop.org/article/10.1088/1742-6596/822/1/012069/pdf DOI : 10.1088/1742-6596/822/1/012069 |
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学科分类:力学,机械学 | |
来源: IOP | |
【 摘 要 】
The Mach-Number series expansion of the potential function for the two dimensional flow of an inviscid, compressible, frozen gas past a circular cylinder are obtained to 29 terms. Analysis of these expansion allows the estimates for the critical Mach-Number M∗, (at which flow first becomes locally Sonic), and the radius of convergence of the series Mcfor the maximum velocity. In this case of two-dimensional circular cylinder we obtain consistent results with 29 terms obtained by Van Dyke and Guttmann [19] for the case of diatomic gas with gamma equal to 7/5. For this case of two dimensions, we have been unable to determine the nature of singularities. We hope this work help to shed a light for resolving the 80-years old conterversary which says that whether the airfoil can posses a continuous range of shock free potential flow above the critical Mach-Number (Mc> M∗).
【 预 览 】
Files | Size | Format | View |
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Analytical solution of subsonic gas flow past a circle | 774KB | download |