Mathematical Modeling of Aerodynamic Heating and Pressure Distribution on a 5-Inch Hemispherical Concave Nose in Supersonic Flow

During the design of an aircraft, a significant parameter that is taken into consideration is aerodynamic heating. Aerodynamically induced heating affects both the structure of the aircraft and its vulnerability to heat-seeking missiles in modern warfare. As a result, the ability to calculate effici...

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Autores principales:	Spiridakos, Dimitrios P., Markatos, Nicholas C., Karadimou, Despoina
Formato:	Capítulo de libro
Lenguaje:	inglés
Publicado:	IntechOpen 2020
Materias:	Physical Sciences, Engineering and Technology
Acceso en línea:	https://www.intechopen.com/chapters/71086
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