Paper Title:
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.

  Info
Periodical
Advanced Materials Research (Volumes 284-286)
Chapter
Other related topics
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, C. H. Zhang, C. G. Zhang, "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
$32.00
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