HLFC后掠翼优化设计的若干问题

来源 :航空学报 | 被引量 : 0次 | 上传用户:njcxm
下载到本地 , 更方便阅读
声明 : 本文档内容版权归属内容提供方 , 如果您对本文有版权争议 , 可与客服联系进行内容授权或下架
论文部分内容阅读
使用扩展自由变形参数化方法,基于径向基函数的动网格技术和改进的混合粒子群算法,考虑吸气的eN转捩预测方法和雷诺平均Navier-Stokes求解器,搭建了针对混合层流流动控制(HLFC)后掠翼的优化设计平台,对HLFC后掠翼的气动外形设计、雷诺数影响、吸气分布设计等多个问题进行了研究,对比分析了在这些因素影响下HLFC后掠翼的阻力系数和层流区长度的差别,进而探索了相应的设计准则.研究表明,对于层流区较长和阻力系数较小的HLFC后掠翼来说,它们上表面的压力分布具有共同的特征:头部峰值较低,之后有一个小的逆压,接下来是一段较长的均匀稳定的顺压,这段顺压最后终结于一道激波.应用HLFC技术后,通过实现大面积的层流区,机翼的摩擦阻力和压差阻力均可显著地降低,降低的幅度远大于不考虑层流控制的设计结果.同时,HLFC机翼的设计应综合考虑摩擦阻力、压差阻力、激波强度和配平阻力(低头力矩),层流区最长不一定意味着阻力最小.一般来说,雷诺数越高,越难维持层流,但应用混合层流控制技术后,即使在难以实现自然层流的高雷诺数下,HLFC机翼依然有较长的层流区.通过对吸气分布的设计进行研究,说明了非均匀吸气比均匀吸气要更有效率一些,能够节省吸气量.“,”An optimization platform is built for the Hybrid Laminar Flow Control (HLFC) sweep wing,based on the extended free-form deformation technique,radial basis function interpolation based mesh deformation,improved particle swarm optimization algorithm,and Reynolds-averaged Navier-Stokes solver coupled with the eN method.Factors about the HLFC wing are researched including airfoil geometry,Reynolds number and suction distribution.The HLFC wing design methodology is discussed by comparing and analyzing how those factors affect the drag coefficient and length of the laminar area.The desired pressure characteristics for the HLFC wing with long laminar area and low drag coefficient are summarized.Results show that the pressure peak at the leading edge is relatively low and followed by a slight adverse pressure gradient,and then a long stable favorable pressure gradient is maintained until a shock wave.After the HLFC technology is applied,a sizable laminar area is obtained,and the friction drag and pressure drag are decreased obviously.Reduction of drag is far greater than the design result without the laminar control.The HLFC design should be based on comprehensive consideration of friction drag,pressure drag,strength of shock and trim drag (nose-down pitching moment).The case with the larger laminar area may not be equivalent to the case with the lowest drag.In general,the higher Reynolds number is,the harder laminar flow is to be maintained.Even though the Reynolds number is too high to maintain the natural laminar flow,the length of the laminar flow is still large if the HLFC technology is applied.Research on suction distribution illustrates that the suction system with variable suction distribution is more efficient for saving suction power compared with the suction system with constant suction distribution.
其他文献
颅脑损伤是基层医院较常见的神经外科疾病,因其病情重,变化快,死亡率高,常给临床救治带来一定的风险和困难.本院2000年1月至2008年12月共收治重型颅脑损伤患者128例,现将救治
为了节省直升机材料研制费用并缩短研发周期,本文试图以理论模拟方法代替腐蚀疲劳试验.试验测定了2种航空铝合金材料LD2CS和LD10CS的预腐蚀疲劳性能,根据试验观测现象和断口
Background:Several studies have revealed that adipose-derived mesenchymal stem cells (ADSCs) can be used as seed cells for the treatment of spinal cord injury (
目的探讨老年甲状腺功能减退症的临床特征及误诊原因。方法对46例老年甲状腺功能减退症患者的资料进行回顾性分析。结果本组误诊24例,其中误诊为冠心病15例,脑梗死3例,老年痴
针对实际问题中经常遇到广义特征值的逆问题,研究了一类对称正定及半正定的左右逆特征问题,给出了这类问题的对称解,对称正定解,对称半正定解存在的充要条件与其解的表达式.
本文优选的"图钉桩"加固高填土路基,是在保护构筑物、填土深度深达29.5m、有大粒径漂石存在于土中、雨季雨水浸渗填土路基而产生沉降的特定条件下,采取的路基加固方案.
期刊
采用反映原子多体相互作用的 FS势模型 ,通过分子动力学方法对液态 Ni3Al的冷却过程进行了研究 ,考察了不同温度下 Ni3Al结构变化特点 .并给出了合金 Ni3Al冷却过程微观结构