Nomogram Analysis of Heat. Transfer in Supersonic Flow: A Method Facilitating the Calculation of Equilibrium and Transient Surface Temperatures for a Turbulent Boundary Layer

Abstract

WHERE computer programmes are not available for the solution of kinetic heating problems, the estimation of equilibrium and transient surface temperatures on bodies in supersonic flow becomes tedious, especially where the transient conditions are to be analysed. A current method of performing these calculations for a turbulent boundary layer is here synthesised into nomogram form.

Citation

Seddon, J. (1961), "Nomogram Analysis of Heat. Transfer in Supersonic Flow: A Method Facilitating the Calculation of Equilibrium and Transient Surface Temperatures for a Turbulent Boundary Layer", Aircraft Engineering and Aerospace Technology, Vol. 33 No. 5, pp. 124-130. https://doi.org/10.1108/eb033407