Heat transfer by radiation from nonisothermal gas stream to hypersonic blunt body is analyzed; relative importance between aerodynamic and radiative heat transfer as function of flight Mach number and altitude is presented; hemispherical emissivity as function of absorption coefficient, nose radius, and standoff distance as parameter is presented in graphical form.
Radiation from nonisothermal gases to stagnation point of hypersonic blunt body
ARS J
ARS Journal ; 32 , n 9
1962
4 pages
Article (Journal)
English
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Stagnation heat flux estimation in spherically blunt axisymmetric hypersonic models
SAGE Publications | 2023
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