基于三维计算流体动力学模拟的隔水管整流罩水动力评估

L. Lai
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摘要

在100,000到1,000,000的雷诺数范围内,整流罩的在线阻力系数(Cdx)约为0.60,这是海上环境的典型特征[1]。最近开发的螺旋槽钻井隔水管浮力在该Re范围内达到了0.65的Cdx值[2],特别是考虑到整流罩的额外安装、存储和维护要求,这是整流罩产品的有力替代品。因此,本文的目的是研究能够实现更低Cdx值的整流罩设计,在这种情况下,整流罩仍然有利于进一步减少阻力载荷。本文提出了一种非平行简化弦马蹄(RCH)整流罩设计,并利用瞬态k-epsilon (reynolds -average Navier-Stokes)湍流模型进行了三维计算流体力学(CFD)分析。建模方法通过先前泪滴型(TD)整流罩设计的两罐测试数据进行了验证,该数据与已发表的同行评审文献非常吻合。研究发现,由于没有整流罩末端效应和整流罩段之间的间隙,使用轴向连续整流罩的CFD模拟人为地提供了较低的Cdx值。从本质上讲,在立管轴向尺寸上无限长且不间断的整流罩是不现实的。与轴向连续整流罩配置相比,结合这种不连续性可以显著增加Cdx。尽管情况如此,但我们发现,对于不连续整流罩配置(假设弦径比为2.0),整个海上Re范围的Cdx可以达到约0.48或更低。更大的弦/直径比将以更长的弦长度为代价提供更低的Cdx,这可能影响整流罩的安装效率。较长的轴向长度也可以获得较低的Cdx,但有颤振不稳定的风险。RCH整流罩设计的这一发展为进一步的整流罩适用于海上钻井作业提供了可能的选择,在海上钻井作业中,除了螺旋槽浮力提供的阻力之外,还需要更低的阻力。
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Drill Riser Fairing Hydrodynamic Assessment With 3-Dimensional Computational Fluid Dynamics Simulations
Fairings have historically been known to achieve in-line drag coefficients (Cdx) of approximately 0.60 across the Reynolds number (Re) range of 100,000 to 1,000,000, typical for the offshore environment [1]. The recent development of helically grooved drill riser buoyancy was shown to achieve Cdx values of 0.65 for this Re range [2], presenting a strong alternative to fairing products especially considering the additional installation, storage and maintenance requirements of fairings. Therefore it is the purpose of this paper to investigate possible fairing designs capable of achieving even lower Cdx values where fairings can still be beneficial in further reducing drag loading. This paper proposes a non-parallel reduced chord horseshoe (RCH) fairing design and is analysed using computational fluid dynamics (CFD) in 3-d using the transient k-epsilon (Reynolds-averaged Navier-Stokes) turbulence model. The modelling approach is validated against tow tank test data of a previous teardrop-shaped (TD) fairing design which showed good agreement with published, peer-reviewed literature. It was found CFD simulations with axially continuous fairings provide artificially low Cdx values due to the absence of fairing end-effects and gaps between fairing sections. In essence, an infinitely long and uninterrupted fairing in the riser axial dimension is not realistic. Incorporation of this discontinuity sees a significant increase in Cdx compared to the axially continuous fairing configuration. Although this is the case, it was found Cdx of approximately 0.48 or lower is achievable for the entire offshore Re range for the discontinuous fairing configuration (assuming a chord/diameter ratio of 2.0). Larger chord/diameter ratios would provide lower Cdx at the cost of a longer chord length which may impact fairing installation efficiency. Longer axial lengths would also achieve lower Cdx but with the risk of flutter instability. This development in RCH fairing design sees a possible option for further fairing applicability to offshore drilling operations where lower drag is desirable beyond that offered by the helically grooved buoyancy.
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