On the calculation of laminar boundary layer on bodies of revolution streamlined by a binary mixture of gases.

Abstract

The paper considers the solution of the laminar boundary layer equations on a semi‑infinite body of revolution streamlined by a binary mixture of gases at zero angle of attack. In the flow and on the surface of the streamlined body a reaction of the type X₂ = 2X is possible. Basic equations and boundary conditions. Consider a high‑temperature boundary layer on a body of revolution with an axis having the direction of the velocity of the oncoming flow. The gas motion in this case is obviously axisymmetric and is completely determined by the flow pattern in the meridional plane.

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