ACCURACY OF CALCULATING THE MOMENTUM-LOSS THICKNESS IN A LAMINAR BOUNDARY LAYER ON THE SURFACE OF A HEMISPHERE IN A SUPERSONIC AIR FLOW

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ACCURACY OF CALCULATING THE MOMENTUM-LOSS THICKNESS IN A LAMINAR BOUNDARY LAYER ON THE SURFACE OF A HEMISPHERE IN A SUPERSONIC AIR FLOW

Volume 90, №3

ACCURACY OF CALCULATING THE MOMENTUM-LOSS THICKNESS IN A LAMINAR BOUNDARY LAYER ON THE SURFACE OF A HEMISPHERE IN A SUPERSONIC AIR FLOW

An engineering method of calculating the momentum-loss thickness in a laminar boundary layer on the surface of a hemisphere is presented based on the approximation of the results of systematic numerical solutions of boundary layer equations.

Author: V. V. Gorskii, V. A. Sysenko, and K. Yu. Dekermendzhi
Keywords: engineering calculation, heat flux, supersonic flow, laminar boundary layer
Page: 535

Link

V. V. Gorskii, V. A. Sysenko, and K. Yu. Dekermendzhi . ACCURACY OF CALCULATING THE MOMENTUM-LOSS THICKNESS IN A LAMINAR BOUNDARY LAYER ON THE SURFACE OF A HEMISPHERE IN A SUPERSONIC AIR FLOW //Journal of engineering physics and thermophysics. . Volume 90, №3. P. 535.

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