Study on Missile Thick Wall Temperature Calculation for Aerodynamic Heat

Bao Zhong Qu; Cheng Hong Zhang; Cheng Guang Zhang

doi:10.4028/www.scientific.net/AMR.284-286.2501

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HomeAdvanced Materials ResearchAdvanced Materials Research Vols. 284-286Study on Missile Thick Wall Temperature...

Study on Missile Thick Wall Temperature Calculation for Aerodynamic Heat

Abstract:

Due to the missile in flight, the airflow temperature around the missile body shall rise and the surface of the missile body shall also be heated. It introduces the engineering calculation method of thick wall aerodynamic heating of the missile, including air flow parameters, heat exchange coefficient and the head surface temperature calculation formula of the missile body.