谢 飞, 叶正寅. 蒙皮波动对飞艇阻力的影响[J]. 工程力学, 2009, 26(1): 250-256.
引用本文: 谢 飞, 叶正寅. 蒙皮波动对飞艇阻力的影响[J]. 工程力学, 2009, 26(1): 250-256.
THE INFLUENCE OF SURFACE FLUCTUATION ON THE DRAG OF THE AIRSHIP[J]. Engineering Mechanics, 2009, 26(1): 250-256.
Citation: THE INFLUENCE OF SURFACE FLUCTUATION ON THE DRAG OF THE AIRSHIP[J]. Engineering Mechanics, 2009, 26(1): 250-256.

蒙皮波动对飞艇阻力的影响

THE INFLUENCE OF SURFACE FLUCTUATION ON THE DRAG OF THE AIRSHIP

  • 摘要: 通过求解雷诺平均Navier-Stokes方程,采用SST两方程湍流模型,研究了蒙皮以不同波长、频率以及波幅作波动时对飞艇流场特性产生的影响。研究结果表明:沿流向蒙皮的波动会引起绕飞艇流场的显著改变。当蒙皮上下表面的波动同相位时,在固定波动幅度和频率条件下,波动的波长减小,流动分离会加剧,时间平均的阻力系数增加;在固定波动波长和频率条件下,波动的波幅增加,流动分离加剧,时间平均的阻力系数增加,而当波幅减小到一定程度时,蒙皮波动对阻力系数基本没有影响;在固定波动波长和幅度条件下,波动频率增加,非定常效应增强,阻力系数减小,甚至出现负值,即可以为飞艇提供推力;此外,适当的波幅和波长组合也可以减小阻力系数。当蒙皮上下表面的波动相位相反时,波长与波幅变化带来的影响与同相位的情况相似;固定波动波长、幅度,波动频率增加,非定常效应增加,由于上下表面的非定常效应是相互抵消的,虽然阻力系数会出现瞬时负值,但是时间平均的阻力系数不会出现负值。

     

    Abstract: Based on the Reynolds-Averaged Navier-Stokes equations with SST turbulent models, this paper studies the flow field around airship with forced envelop fluctuation, and concludes that the fluctuation of the envelop can cause significant change of the flow field. 1) When the upper and lower envelop are in the same phase, the decrease on wavelength can prick up the separation, and the time-averaged drag coefficient increases; 2) the drag coefficient increases with the increase of the fluctuation amplitude; 3) If the fluctuation amplitude is small, the wavelength has no effect no matter how small it is; 4) large frequency can induce serious unstability, and decrease drag coefficient; 5) the proper combination of wavelength and amplitude can decrease drag coefficient; 6) when the upper and lower envelop are in converse phase, the effects of wavelength and amplitude are similar to the case of same phase; 7) due to the offset of the upper and lower envelop, the time dependent drag coefficient may be negative temporally, but the time-averaged drag coefficient keeps positive.

     

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