On Shock Layer Method for the Hypersonic Flow Problems

Yuan Yi-wu

Volume 8 Issue 5

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Abstract

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Article Navigation > Applied Mathematics and Mechanics > 1987 > 8(5): 453-462

Yuan Yi-wu. On Shock Layer Method for the Hypersonic Flow Problems[J]. Applied Mathematics and Mechanics, 1987, 8(5): 453-462.

Citation:

Yuan Yi-wu. On Shock Layer Method for the Hypersonic Flow Problems[J]. Applied Mathematics and Mechanics, 1987, 8(5): 453-462.

Citation:

Yuan Yi-wu. On Shock Layer Method for the Hypersonic Flow Problems[J]. Applied Mathematics and Mechanics, 1987, 8(5): 453-462.

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On Shock Layer Method for the Hypersonic Flow Problems

Yuan Yi-wu

South-Central University of Technology, Changsha

Received Date: 1985-04-21
Publish Date: 1987-05-15

Abstract

Abstract

Chernyi's series method is not proper for the case that(γ-l)/(γ+l)<<2/(γ+1)(M²sin²β)(γ=c_p/c_v-adiabatic index number, M-Much number, shock incidence). In this paper, we only suppose that in the neighbour of the shock, there exists a shock layer in which the density of the gas is very big, but we do not remove the case that (γ-1)/(γ+1)<<2/(γ+1)(M²sin²β).

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References(4)

References

[1]	Черный Г.Г.,Теченuя Газа с Болъuоu Сберхзбуковоu Скоросmыо,(1959)125-139.
[2]	Швец М.Е.,О Приближенном решении некоторых залач гидродинамики пограничного слоя,ПММ.,3(1949),257-266.
[3]	Аржаников Н.С.,Г.С.Садекова,Азробuнамuка Болошuх Скоросmеu(1965).373-380.
[4]	复旦大学数学系编,《流体力学》(1860), 521.

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