On the equations of supersonic three-dimensional flows of a nonviscous gas
Authors:
Abstract
In the study of some problems of streamline bodies with supersonic gas flow, it is more convenient to write down the system of hydromechanics equations in natural coordinates rather than in Cartesian coordinates. Similar coordinates were used in solving problems of the flow of flat and axisymmetric bodies with hypersonic gas flow by the “boundary layer” method.
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(Archived) Without section
References
- Honore A. L. Streamline of a cone at an angle of attack with a large supersonic velocity. Proc. of the Academy of Sciences of the USSR, OTN, Mechanics and Mechanical Engineering, No. 7, 1958.
- Kochin N. Е. Vector calculus and the beginnings of tensor calculus. PH of the AS USSR, 1961.
- Freeman N. Toward a Theory of Hypersonic Flow Streaming Flat and Axisymmetric Bodies. In the collection: Problems of Motion of the Head Part of Long-Range Rockets. FL, 1959.
- Cherny G. G. Currents of Gas with Large Supersonic Velocity. Fizmatgiz, 1959.
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