Flow about Cones at Very High Speeds

Author:

Zienkiewicz H. K.

Abstract

Summary:Effects of vibrational excitation and dissociation of air on inviscid high speed flow past a circular cone, at zero incidence, with an attached shock wave, are studied on the assumption of thermal equilibrium. A numerical solution of the problem is outlined and an approximate analytic solution for the flow between the surface of the cone and the shock wave is developed. Two numerical examples are given as an illustration and compared with the corresponding solutions assuming constant air properties.

Publisher

Cambridge University Press (CUP)

Subject

General Engineering

Cited by 12 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. The Victoria University of Manchester’s contributions to the development of aeronautics;The Aeronautical Journal;2007-08

2. Dissociation effect on the hypersonic flow past a circular cylinder;Proceedings of the Indian Academy of Sciences - Section A;1966-06

3. Dissociation effects in hypersonic flow past a circular cone at an angle of attack;Proceedings of the Indian Academy of Sciences - Section A;1966-03

4. Effects of dissociation or ionization on hypersonic flow past a cone;Proceedings of the Indian Academy of Sciences - Section A;1965-08

5. Calculation of hypersonic flow over bodies of revolution at small angles of attack;AIAA Journal;1965-03

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