IHS ESDU Heat transfer definitions and equations. 89022

Description
ESDU 89022 defines quantities and gives equations required in estimating the temperature of a structure due to aerodynamic heating. The terms are specific heat capacity, thermal conductivity, thermal diffusivity, emissivity, absorptivity, heat transfer coefficient, Biot number, stagnation temperature, and recovery temperature and factor. The equation is given for the equilibrium skin temperature under aerodynamic heating allowing for radiation heating both to and from the structure, and its applicability to thin skins in which no temperature gradient exists is considered. The case of thick skins is also considered, and methods of determining the temperature distribution under various simplifying assumptions are discussed.
Description
ESDU 89022 defines quantities and gives equations required in estimating the temperature of a structure due to aerodynamic heating. The terms are specific heat capacity, thermal conductivity, thermal diffusivity, emissivity, absorptivity, heat transfer coefficient, Biot number, stagnation temperature, and recovery temperature and factor. The equation is given for the equilibrium skin temperature under aerodynamic heating allowing for radiation heating both to and from the structure, and its applicability to thin skins in which no temperature gradient exists is considered. The case of thick skins is also considered, and methods of determining the temperature distribution under various simplifying assumptions are discussed.

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Heat transfer definitions and equations. - 89022 - IHS ESDU
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Heat transfer definitions and equations.
89022
Heat transfer definitions and equations. 89022
ESDU 89022 defines quantities and gives equations required in estimating the temperature of a structure due to aerodynamic heating. The terms are specific heat capacity, thermal conductivity, thermal diffusivity, emissivity, absorptivity, heat transfer coefficient, Biot number, stagnation temperature, and recovery temperature and factor. The equation is given for the equilibrium skin temperature under aerodynamic heating allowing for radiation heating both to and from the structure, and its applicability to thin skins in which no temperature gradient exists is considered. The case of thick skins is also considered, and methods of determining the temperature distribution under various simplifying assumptions are discussed.

ESDU 89022 defines quantities and gives equations required in estimating the temperature of a structure due to aerodynamic heating. The terms are specific heat capacity, thermal conductivity, thermal diffusivity, emissivity, absorptivity, heat transfer coefficient, Biot number, stagnation temperature, and recovery temperature and factor. The equation is given for the equilibrium skin temperature under aerodynamic heating allowing for radiation heating both to and from the structure, and its applicability to thin skins in which no temperature gradient exists is considered. The case of thick skins is also considered, and methods of determining the temperature distribution under various simplifying assumptions are discussed.

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Technical Specifications

  IHS ESDU
Product Category Standards and Technical Documents
Product Number 89022
Product Name Heat transfer definitions and equations.
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