Abstract
The Newtonian shock layer theory for smooth surfaces has been developed in [1–7]. However, if a body consists of two intersecting surfaces, on each of which there is a regular shock layer, these two layers will interact at the line of intersection. Considering that the shock layer is hypersonic, we can again apply the Newton scheme to the impact of the particles with the second surface. As a result, concentrated forces arise at the line of intersection. An indication of the possibility of the appearance of such forces is given in [2]. In the following we present a method of calculating the concentrated forces and indicate the real flow of which they are the analogy.
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References
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Gonor, A.L. The Newton drag law for bodies formed by intersecting surfaces. Fluid Dyn 2, 61–65 (1967). https://doi.org/10.1007/BF01024805
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DOI: https://doi.org/10.1007/BF01024805