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On the accuracy of engineering methods for calculation
of specific heat flow in laminar boundary layer
on non-permeable “wall” of hemisphere surface
in a supersonic gas flow
© V.V. Gorsky
1,2
, V.A Sysenko
1
, A.A Blokhina
2
1
JSC MIC "NPO Mashinostroenia", Reutov town, 143966, Russia
2
Bauman Moscow State Technical University, Moscow, 105005, Russia
The research explored engineering methods for specific heat flow calculation in laminar
boundary layer on non-permeable “wall” of hemisphere surface in a supersonic gas
flow. In this paper we present the results of examining these methods and estimating their
accuracy. The study delves into the ways of solving the problem, proposed by I.N. Murzi-
nov and offers a similar engineering technique of high accuracy in accordance with
modern scientific and technological achievements. Consequently, we to large extent ex-
panded the variation range of such determining factors as Mach number in the incoming
air stream, the brake pressure of this flow, enthalpy.
Keywords
: specific heat flow, supersonic gas flow, laminar boundary layer, engineering
methods.
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