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提高进气道冲压阻力测量精度的方法 被引量:1
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作者 雷杰 雷晓波 +1 位作者 申世才 张晓飞 《科学技术与工程》 北大核心 2019年第18期334-339,共6页
为提高发动机飞行推力测量精度,对进气道冲压阻力测量计算方法进行了研究。鉴于进气道测量耙总压静压测点不遵循等环面分布,采用数值插值法获得等环面中心点的总压静压值,计算表明:靠近壁面的实际测点与其对应的等环面中心点之间的总压... 为提高发动机飞行推力测量精度,对进气道冲压阻力测量计算方法进行了研究。鉴于进气道测量耙总压静压测点不遵循等环面分布,采用数值插值法获得等环面中心点的总压静压值,计算表明:靠近壁面的实际测点与其对应的等环面中心点之间的总压静压差异明显,总压最大差值为 1. 0 kPa,静压最大差值为 0. 73 kPa。分析了附面层厚度、分区域计算累加法、全区域计算平均法对流量、流速、冲压阻力的影响,结果表明:附面层造成的空气流量最大误差值可达1. 94 kg/s,差异较明显;采用分区域计算累加法与采用全区域总压静压平均值计算的空气流量差异小。采用分区域计算累加法与采用全区域总压静压平均值计算的冲压阻力最大差值仅为 0. 09 kN,差异很小,两种方法在推力直接确定中都具有应用价值。 展开更多
关键词 飞行推力 推力直接确定 进气道冲压阻力 测量精度 空气流量 附面层
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动力模拟风洞试验中标准推阻分解方法的适用性分析
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作者 陈莹 巴玉龙 +1 位作者 王奇志 郭传亮 《民用飞机设计与研究》 2018年第4期24-28,共5页
从标准推阻分解方法(Standard-Bookkeeping-Method,简称SBM)的原理出发,分析了该方法在不同发动机模拟状态下的适用性。当发动机风扇压比高、喷管流动达到超音速(壅塞)状态时,动力模拟试验采用SBM方法计算质量流量和推力,其结果是正确的... 从标准推阻分解方法(Standard-Bookkeeping-Method,简称SBM)的原理出发,分析了该方法在不同发动机模拟状态下的适用性。当发动机风扇压比高、喷管流动达到超音速(壅塞)状态时,动力模拟试验采用SBM方法计算质量流量和推力,其结果是正确的;当发动机风扇压比低、喷管流动为亚声速流动状态时,此时质量流量和动力模拟器的推力计算与外涵出口平面处的静压相关,SBM方法中喷口处静压Pe与前方来流静压P0相等的假设,导致计算中引入误差从而影响动力干扰分析。文中给出了不同静压差引起的质量流量和推力误差量,表明在动力模拟风洞试验中应测量外涵出口平面处的静压以获得可靠的动力干扰量。 展开更多
关键词 涡轮动力模拟器 标准推阻分解方法 风洞试验 冲压阻力
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Study on the resistance spot welding technology of 22MnMoB hot stamping quenched steel 被引量:2
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作者 Feng Yi Ma Mingtu +3 位作者 Hua Fu'an Zhang Junping Song Leifeng Jin Qingsheng 《Engineering Sciences》 EI 2014年第5期45-53,共9页
In this paper, the spot welding technology of a new kind of 22MnMoB hot stamping quenched steel sheet was systematically studied by power frequency spot welder. Through a series of technology and test experiments, we ... In this paper, the spot welding technology of a new kind of 22MnMoB hot stamping quenched steel sheet was systematically studied by power frequency spot welder. Through a series of technology and test experiments, we have obtained the optimal spot welding technological parameter condition. According to the results, the relations among spot welding technological parameter, welding nugget, mechanical property and fracture mode were discussed. The effects of all the welding parameters such as welding current, welding time and electrode force on the quality of joint can be boiled down to one thing--the diameter of welding nugget. The experimental results showed that welding nugget diameter determines the mechanical property of spot welding joint and the relation between welding nugget diameter and the mechanical property of joint presents a kind of linear mathematic representation. There are two typical fracture models of 22MnMoB hot stamping quenched steel sheet, i.e., interracial fracture and nugget pullout. Other than mild steel or normal high strength steel, in the shearing tensile test, hot stamping quenched steel has a great tendency to fail in interfacial mode due to the effects of high strength matrix structure, welding soft zone and the porosity level of fusion zone. 展开更多
关键词 hot stamping quenched steel resistance spot welding maximum shearing force nugget diameter soft zone fracture mode
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Drag force investigation of cavities with different geometric configurations in supersonic flow 被引量:1
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作者 LUO ShiBin HUANG Wei +1 位作者 LIU Jun WANG ZhenGuo 《Science China(Technological Sciences)》 SCIE EI CAS 2011年第5期1345-1350,共6页
In order to prolong the residence time of the flow retaining in the supersonic flow, wall cavity has been widely applied in the scramjet combustor, and this affects the aerodynamic surface and imposes additional drag ... In order to prolong the residence time of the flow retaining in the supersonic flow, wall cavity has been widely applied in the scramjet combustor, and this affects the aerodynamic surface and imposes additional drag force on the hypersonic propulsion system. The two-dimensional coupled implicit Reynolds Averaged Navier-Stokes (RANS) equations and the RNG k?ε turbulent model were employed to investigate the flow fields of cavities with different geometric configurations, namely the classical rectangular, triangular and semi-circular, and the cavities with the fixed depth and length-to-depth ratio. At the same time, the drag force performances of the cavities were estimated and compared. The obtained results show that the numerical results are in very good agreement with the experimental data, and the different scales of grid make only a slight difference from the numerical results. The intensity of the trailing shock wave is much stronger than that of the leading one, and the area around the trailing edge of the cavities plays an important role in the chemical reaction in the scramjet combustor. With the fixed depth and length-to-depth ratio, the triangular cavity can strengthen the turbulent combustion in the scramjet combustor further, but impose the most additional drag force on the scramjet engine. The classical rectangular one can impose the least additional drag force on the engine, but the function of strengthening the combustion is the weakest. The influence of the semi-circular one is the moderate, but the machining process is more complex than the other two configurations. 展开更多
关键词 aerospace propulsion systems CAVITY drag force scramjet engine hypersonic vehicle
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