检索规则说明:AND代表“并且”;OR代表“或者”;NOT代表“不包含”;(注意必须大写,运算符两边需空一格)
检 索 范 例 :范例一: (K=图书馆学 OR K=情报学) AND A=范并思 范例二:J=计算机应用与软件 AND (U=C++ OR U=Basic) NOT M=Visual
作 者:汪鹏程 洪亮[1] 陈海斌 WANG Pengcheng;HONG Liang;CHEN Haibin(School of Energy and Power Engineering,Nanjing University of Science&Technology,Nanjing 210094,China;Taizhou City Jinhaiyun Vessel Facility Co.,Ltd.,Taizhou 225324,China)
机构地区:[1]南京理工大学能源与动力工程学院,南京210094 [2]泰州市金海运船用设备有限责任公司,江苏泰州225324
出 处:《兵器装备工程学报》2024年第4期67-74,146,共9页Journal of Ordnance Equipment Engineering
基 金:江苏省工业和信息产业转型升级专项资金项目(696785044)。
摘 要:全垫升气垫船动力和阻力的计算和匹配问题的研究是其设计前期阶段的关键。基于STAR-CCM+流体计算平台和滑移网格模型分别对空投气垫船水面航行过程和螺旋桨气动特性进行了数值模拟,得到不同航速下的航行阻力和螺旋桨推力数据,综合分析研究了两者的匹配性问题。研究结果表明:兴波阻力随航速变化趋势和阻力峰出现位置均与相关文献和试验数据吻合,验证螺旋桨的推力计算结果与试验误差在6%以内,验证了CFD方法对气垫船航行阻力及螺旋桨动力模拟计算的可行性与有效性;将2款待选用的四叶和三叶螺旋桨气动性能与航行阻力匹配分析后,在发动机极限性能转速下,三叶螺旋桨能达到更高的最大航速,以20节速率巡航时,三叶效率更高,同时质量轻15%,综合说明三叶螺旋桨性能更佳。研究结果为该型气垫船的设计和选型提供重要的理论依据与数据支撑。The study on the calculation and matching of the power and resistance of the hovercraft is the key in the early stage of its design.Based on STAR-CCM+fluid computing platform and sliding grid model,the surface navigation process and propeller aerodynamic characteristics of air dropped Hovercraft are simulated respectively.The simulations provide data on the navigation resistance and propeller thrust at different speeds,and a comprehensive analysis is performed to investigate their matching relationship.The study results show that the wave-making resistance exhibited a changing trend with the speed and the location of the resistance peak aligned with relevant literature and experimental data.The calculated propeller thrust is verified to have an error of less than 6%compared to experimental results,confirming the feasibility and effectiveness of using computational fluid dynamics(CFD)methods for simulating the navigation resistance and propeller dynamics of air cushion vehicles.After conducting a matching analysis between the performance of two candidate propellers,a four-blade and a three-blade propeller,with the navigation resistance,it is found that at the engine’s maximum performance speed,the three-blade propeller could achieve a higher maximum speed.When cruising at a speed of 20 knots,the three-blade propeller exhibits higher efficiency and was 15%lighter,indicating superior performance.Thus,the study demonstrates the better performance of the three-blade propeller.The study results provide important theoretical basis and data support for the design and selection of this type of hovercraft.
分 类 号:U661.1[交通运输工程—船舶及航道工程]
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在链接到云南高校图书馆文献保障联盟下载...
云南高校图书馆联盟文献共享服务平台 版权所有©
您的IP:216.73.216.38