Study on Missile Thick Wall Temperature Calculation for Aerodynamic Heat

Abstract:

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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.

Info:

Periodical:

Advanced Materials Research (Volumes 284-286)

Main Theme:

Edited by:

Xiaoming Sang, Pengcheng Wang, Liqun Ai, Yungang Li and Jinglong Bu

Pages:

2501-2504

DOI:

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

Citation:

B. Z. Qu et al., "Study on Missile Thick Wall Temperature Calculation for Aerodynamic Heat", Advanced Materials Research, Vols. 284-286, pp. 2501-2504, 2011

Online since:

July 2011

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Price:

$35.00

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