共查询到18条相似文献,搜索用时 234 毫秒
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二维地效翼气动力的计算和性能研究 总被引:5,自引:0,他引:5
本文基于势流边界元理论(BEM)和边界层动量积分关系式数值求解二维地铲翼的气动力,研究了升力正负地效问题及粘性对地效翼升力、俯仰力矩及焦点的影响,并给出了不同地面边界条件的计算结果及相应的粘性修正方法。 相似文献
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本文提出了一种可以较精确地计算地效翼船巡航状态下气动力的设计方法,应用流体力学中线性和非线性湍流理论并结合有限元法对地效翼船进行了气动性能计算,并结合实验数据对比,可以发现应用非线性湍流理论计算值较为精确.同时又将单算主翼气动性能与计算整体地效翼船数值进行对比,发现单算的主翼气动力大于整体算法的,这主要是未考虑主浮舟等附体对气动力的贡献.作为设计之初可以考虑单算主翼,但随着工作的深入一定要对地效翼船整体气动力性能进行研究,以确定巡航状态下是否提供足够的升力,这是地效翼船设计的关键.在进行整体和单体计算后又进行了不同高度下的气动力分析,分析表明随高度增大地效翼船升力明显减少,并得出适合地效翼船巡航的高度. 相似文献
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《中国舰船研究》2020,(4)
[目的]在复合材料地效翼船的结构设计中,目前尚无相应的对其结构进行强度和稳定性评估的规范方法。选取复合材料地效翼船设计中夹芯复合材料主浮舟及机翼这2个关键部件的结构强度及稳定性计算方法开展研究。[方法]重点探讨主浮舟及机翼结构的设计载荷计算方法,以及对应夹芯板的强度衡准、整体及局部稳定性计算方法与衡准。利用建立的计算方法对复合材料地效翼船主浮舟的总纵弯曲强度、机翼结构强度以及稳定性进行算例分析。[结果]结果表明,建立的计算方法可以用于复合材料地效翼船主浮舟和机翼结构的强度及稳定性计算,算例中的复合材料地效翼船设计方案满足结构强度和稳定性要求,经受住了实船试验的考核验证。[结论]所得方法可供复合材料地效翼船结构设计计算参考。 相似文献
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Omer Kemal Kinaci 《船舶与海洋工程学报》2016,15(2):136-143
Aircraft flying close to the ground benefit from enhanced efficiency owing to decreased induced drag and increased lift. In this study, a mathematical model is developed to simulate the takeoff of a wing near the ground using an Iterative Boundary Element Method (IBEM) and the finite difference scheme. Two stand-alone sub-codes and a mother code, which enables communication between the sub-codes, are developed to solve for the self-excitation of the Wing-In-Ground (WIG) effect. The aerodynamic force exerted on the wing is calculated by the first sub-code using the IBEM, and the vertical displacement of the wing is calculated by the second sub-code using the finite difference scheme. The mother code commands the two sub-codes and can solve for the aerodynamics of the wing and operating height within seconds. The developed code system is used to solve for the force, velocity, and displacement of an NACA6409 wing at a 4° Angle of Attack (AoA) which has various numerical and experimental studies in the literature. The effects of thickness and AoA are then investigated and conclusions were drawn with respect to generated results. The proposed model provides a practical method for understanding the flight dynamics and it is specifically beneficial at the pre-design stages of a WIG effect craft. 相似文献
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An optimization technique was used to generate a wing-in-ground-effect (WIG) configuration which can achieve the maximum lift
and satisfy the height stability criteria within the design constraints. For the analysis of the aerodynamic coefficients,
the vortex lattice method (VLM) was applied with the inviscid and potential flow approximations. The sequential quadratic
programming (SQP) method, which is a nonlinear optimization method, was employed as an optimization tool. The lift and moment
coefficients, including the stability analysis computed by VLM, were compared with the experimental results of a medium-sized
WIG, and a good correlation was found between them. In addition, the optimization tool was validated by finding the optimal
position of the side wing attached on the WIG craft. Then, various optimum examples are shown, with generation of the wing
section, the determination of the planform configuration, the aspect ratio, and the position of the tail wing within the design
constraints. It was shown that the present optimization tool can be used effectively for the optimal design of a WIG craft. 相似文献
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对三峡坝区下游的黄陵庙至南津关长约28.5 km的河段进行了一维和二维非恒定流数值模拟。文中采用Presimann四点偏心隐式差分求解一维非恒定流,采用正交曲线坐标系下二维水深平均数学模型进行二维非恒定流计算。根据实测资料,由河段上、下游的黄陵庙、南津关(二)水位站测定的水位过程给定水位边界条件,通过河段中的莲沱、石牌、平善坝水位站的实测水位过程以及黄陵庙(陡)水文站实测的流量过程进行模型验证,结果表明一维和二维数模计算出的水位、流量过程与实测值符合良好。由于二维计算时间远大于一维,因此在拟定和优化三峡—葛洲坝联合调峰运行方案时可主要采用一维非恒定流模型,在某些工况下,因通航限制而需要限定局部河段流速时可采用二维非恒定流模型。 相似文献
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