201. Numerical Computation for High Speed Aerodynamic Heat Transfer on the Axisymmetric Configuration.
- Author
-
Kai-Long Hsiao
- Subjects
AERODYNAMIC heating ,HEAT convection ,HEAT flux ,HEAT conduction ,NUMERICAL calculations ,HEAT transfer ,MECHATRONICS - Abstract
The study provides a numerical calculation for convection coefficients and heat fluxes due to aerodynamic heating on hypersonic vehicle which are obtained analytically and computationally for protection some thermal mechatronics systems. The heat transfer through a thin, a thick wall were analyzed in the present study. Convection coefficients and heat fluxes due to aerodynamic heating on critical surfaces of hypersonic vehicle are obtained analytically. The applicability of recovery temperature for axisymmetric configuration regions is discussed. Convection coefficient for the axisymmetric configuration region is obtained directly from axisymmetric region correlation. This paper shows and application of Crank-Nicolson scheme to solve numerically transient heat conduction problem conjugate with high speed aerodynamic heating problem. The results show good agreement with a known Lumped system method solution for a thin wall. Finally, it can use to the material design for the high speed flying body. [ABSTRACT FROM AUTHOR]
- Published
- 2023