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chunk-278d5570.32e3f8b9.js

chunk-278d5570.32e3f8b9.js 5.9 KB
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(window["webpackJsonp"]=window["webpackJsonp"]||[]).push([["chunk-278d5570"],{"0b86":function(t,s,a){},2064:function(t,s,a){"use strict";a.r(s);var i=function(){var t=this,s=t.$createElement,i=t._self._c||s;return i("DetailLayout",{attrs:{title:"前沿-HCFDLab-Agard Wing升阻力曲线分析"}},[i("div",{staticClass:"detail"},[i("div",{staticClass:"content-left"},[i("p",{staticClass:"title"},[t._v("计算目标：")]),t._v(" "),i("p",{staticClass:"dec"},[t._v("\n          Agard\n          445.6薄翼型机翼在0.678、0.901和1.141三个马赫数下的升力阻力曲线。\n        ")]),t._v(" "),i("div",[i("p",{staticClass:"title"},[t._v("模型参数:")]),t._v(" "),i("p",{staticClass:"dec"},[t._v("图1 Agard-wing 445.6的平面图")]),t._v(" "),i("div",{staticClass:"imgs"},[i("img",{attrs:{src:a("9ec6"),alt:"图片"}})]),t._v(" "),i("p",{staticClass:"dec"},[t._v("表 1 Agard-wing 445.6的几何尺寸")]),t._v(" "),i("table",{staticClass:"dec",attrs:{border:"0.1"}},[i("tr",[i("td",[t._v("Mass (kg)")]),t._v(" "),i("td",[t._v("2.3786")])]),t._v(" "),i("tr",[i("td",[t._v("Root chord 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"),i("td",[t._v("0.07836")])])]),t._v(" "),i("p",{staticClass:"title"},[t._v("网格格式:")]),t._v(" "),i("p",{staticClass:"dec"},[t._v("\n            非结构流体软件HCFDLab支持四面体、金字塔、三棱柱、六面体等多种网格类型，这种非结构化网格，无论气动外形复杂度有多高，都可以方便、快速地进行网格划分，并根据用户需要和实际外形特点对模型进行分块（part）。用网格生成软件（如ICEM或PointWise）划分好整个流场的网格后，导出\n            .ugrid 格式网格文件，HCFDLab可直接读入此类型的网格文件，在导出\n            .ugrid 格式网格文件时会同时生成 .dat\n            格式的边界文件，这两个文件一起构成非结构气弹模块流场分析准备文件。目前，HCFDLab只支持这一种网格文件类型。\n          ")])])]),t._v(" "),i("div",{staticClass:"content-right"},[i("p",{staticClass:"title"},[t._v("相关资料")])])])])},e=[],n=a("97f2"),c={name:"Detailaw",components:{DetailLayout:n["a"]},data:function(){return{}},created:function(){},mounted:function(){},methods:{}},v=c,d=(a("fd38"),a("2877")),r=Object(d["a"])(v,i,e,!1,null,"76cb4bf0",null);s["default"]=r.exports},"31cc":function(t,s,a){},"97f2":function(t,s,a){"use strict";var i=function(){var t=this,s=t.$createElement,i=t._self._c||s;return i("div",{staticClass:"details"},[t._m(0),t._v(" 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