Initial Missile Ballistic Analysis Under the Condition of the Interference of a Helicopter's Rotor Down-wash Flow

WEI Jing-biao;ZHENG Hua-Ii

Acta Armamentarii ›› 2006, Vol. 27 ›› Issue (6) : 1129-1131. DOI: 10.3969/j.issn.1000-1093.2006.06.040
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Initial Missile Ballistic Analysis Under the Condition of the Interference of a Helicopter's Rotor Down-wash Flow

  • WEI Jing-biao1, ZHENG Hua-Ii2
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Abstract

Combining momentum theory and vortex theory, rotor circulation equation was deduced. The rotor down-wash flow field was calculated using generalized down-wash flow model. On this ba?sis, the initial missile trajectory was calculated on both the conditions with and without rotor down- wash flow. The result indicates that the rotor down-wash flow has an obvious influence on the initial missile trajectory.

Key words

fluid mechanics / circulation equation / rotor down-wash flow / aerodynamic interference / initial trajectory

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WEI Jing-biao, ZHENG Hua-Ii. Initial Missile Ballistic Analysis Under the Condition of the Interference of a Helicopter's Rotor Down-wash Flow. Acta Armamentarii. 2006, 27(6): 1129-1131 https://doi.org/10.3969/j.issn.1000-1093.2006.06.040

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