找回密碼
 To register

QQ登錄

只需一步,快速開(kāi)始

掃一掃,訪問(wèn)微社區(qū)

12345
返回列表
打印 上一主題 下一主題

Titlebook: EUROPT — A European Initiative on Optimum Design Methods in Aerodynamics; Proceedings of the B Jacques Periaux,Gabriel Bugeda,Bruno Stouffl

[復(fù)制鏈接]
41#
發(fā)表于 2025-3-28 14:38:53 | 只看該作者
42#
發(fā)表于 2025-3-28 19:50:23 | 只看該作者
43#
發(fā)表于 2025-3-29 00:20:53 | 只看該作者
Single-Pass Method for the Solution of the 2-D & 3-D Inverse Potential Problemtions of the grid lines, after the flow field has been determined. The 2-D case is treated as a particular case of the general 3-D one. The method has been applied to both 2-D and 3-D reproduction cases of the present workshop with very satisfactory results.
44#
發(fā)表于 2025-3-29 05:21:52 | 只看該作者
45#
發(fā)表于 2025-3-29 07:28:12 | 只看該作者
Contribution to Problems T4 and T6 Finite Element GMRES and Conjugate Gradient Solversf airfoils represented by cubic splines and operating at subsonic and transonic conditions. It is shown that the number of iterations has been multiplied by three between the subsonic and the transonic case. For the optimization problem, the drag objective function is penalized to take into account
46#
發(fā)表于 2025-3-29 13:31:57 | 只看該作者
Wing Design with a 3D-Subsonic Inverse Panel Method: ’design patches’, whose surface is derived from given pressures and ’analysis patches’, whose pressures are derived from given surface. To solve such ’mixed’ problems the panel code is embedded into an iteration loop, which minimizes the sum of squared pressure deviations. The geometry representat
47#
發(fā)表于 2025-3-29 18:32:19 | 只看該作者
A Residual Correction Method Applied to 2D Multi-Point Airfoil Design and 3D Single-Point Wing Desigd is based on full-potential theory and minimizes a cost function weighting the deviations from specified target pressure distributions for each design condition in a least squares sense. Deviations from specified target pressure distributions (residuals) are translated into airfoil geometry correct
48#
發(fā)表于 2025-3-29 22:59:17 | 只看該作者
49#
發(fā)表于 2025-3-30 02:37:16 | 只看該作者
Aerodynamic Shape Optimization Using Automatic Adaptive Remeshingzed by the Finite Element Method. A suitable and very general technique for the parametrization of the optimization problem using B-splines to define the boundary is first presented. Then, mesh generation using the advancing front method, the estimation of error and the mesh refinement criterion are
50#
發(fā)表于 2025-3-30 07:52:05 | 只看該作者
12345
返回列表
 關(guān)于派博傳思  派博傳思旗下網(wǎng)站  友情鏈接
派博傳思介紹 公司地理位置 論文服務(wù)流程 影響因子官網(wǎng) 吾愛(ài)論文網(wǎng) 大講堂 北京大學(xué) Oxford Uni. Harvard Uni.
發(fā)展歷史沿革 期刊點(diǎn)評(píng) 投稿經(jīng)驗(yàn)總結(jié) SCIENCEGARD IMPACTFACTOR 派博系數(shù) 清華大學(xué) Yale Uni. Stanford Uni.
QQ|Archiver|手機(jī)版|小黑屋| 派博傳思國(guó)際 ( 京公網(wǎng)安備110108008328) GMT+8, 2025-10-23 13:50
Copyright © 2001-2015 派博傳思   京公網(wǎng)安備110108008328 版權(quán)所有 All rights reserved
快速回復(fù) 返回頂部 返回列表
双牌县| 渭南市| 吉木萨尔县| 舟曲县| 万安县| 疏附县| 江西省| 长乐市| 青龙| 苗栗县| 夏津县| 云霄县| 芦溪县| 蕲春县| 定陶县| 晋江市| 富裕县| 民乐县| 武胜县| 商城县| 舒城县| 南涧| 桑日县| 仙桃市| 商洛市| 桃江县| 阳城县| 定西市| 佳木斯市| 广南县| 岳阳县| 丰台区| 苏尼特左旗| 蒙城县| 齐河县| 安平县| 盐津县| 萝北县| 鄂托克旗| 泰和县| 马鞍山市|