Study on Missile Thick Wall Temperature Calculation for Aerodynamic Heat
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.
Xiaoming Sang, Pengcheng Wang, Liqun Ai, Yungang Li and Jinglong Bu
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