找回密码
 To register

QQ登录

只需一步,快速开始

扫一扫,访问微社区

Titlebook: Variational Analysis and Aerospace Engineering; Giuseppe Buttazzo,Aldo Frediani Conference proceedings 2009 Springer-Verlag New York 2009

[复制链接]
楼主: bile-acids
发表于 2025-3-28 15:40:44 | 显示全部楼层
发表于 2025-3-28 22:31:59 | 显示全部楼层
发表于 2025-3-29 00:13:18 | 显示全部楼层
Algorithm Issues and Challenges Associated with the Development of Robust CFD Codes,ject aerodynamicists need access to tools that accurately predict and confirm vehicle flight characteristics. Thirty years ago, these tools consisted almost entirely of analytic approximation methods, wind tunnel tests, and flight tests.With the development of increasingly powerful computers, numeri
发表于 2025-3-29 05:08:06 | 显示全部楼层
Flight Path Optimization at Constant Altitude,range of a turbofan powered aircraft. Most analyses of optimal transport aircraft flight begin with the assumption that the flight profile consists of three segments – climb, cruise and descent. Indeed, this is the flight profile of all long-haul commercial flights today. The dominant stage of such
发表于 2025-3-29 07:17:45 | 显示全部楼层
发表于 2025-3-29 14:34:23 | 显示全部楼层
Innovative Rotor Blade Design Code,ruise speed and higher cruise altitude, but, at the same time, guaranteeing the maximum level of comfort for the crew and the passengers. To achieve this goal, it is normal practice to apply some design rules to the rotor aeromechanic behaviour but the residual hub loads transferred to the supportin
发表于 2025-3-29 19:31:53 | 显示全部楼层
Fields of Extremals and Sufficient Conditions for the Simplest Problem of the Calculus of Variationt problem of the calculus of variations. Subsequently, in a series of papers, starting in 2001, he revived this approach and extended it in a variety of ways. Shortly thereafter, Carlson presented an important generalization of this approach and connected it to Carathéodory’s equivalent problem meth
发表于 2025-3-29 21:06:39 | 显示全部楼层
A Framework for Aerodynamic Shape Optimization,ured finite-volume formulation for the solution of the Euler equations and a discrete adjoint method for the computation of the sensitivity. The framework is demonstrated on 2D and 3D shape optimization problems for which the drag coefficient must be minimized, the lift coefficient must be kept cons
发表于 2025-3-30 01:36:26 | 显示全部楼层
Optimal Motions of Multibody Systems in Resistive Media,dy. In this chapter, progressive motions of a body carrying movable internal masses are considered for various resistance forces acting upon the body. The cases of linear and quadratic resistance as well as Coulomb’s dry friction forces, both isotropic and anisotropic, are analyzed. Special classes
发表于 2025-3-30 04:41:13 | 显示全部楼层
,Instationary Heat-Constrained Trajectory Optimization of a Hypersonic Space Vehicle by ODE–PDE-Consreme aerothermic loads. Therefore, an efficient, sophisticated and lightweight thermal protection system is determinative for the success of the entire mission. For a deeper understanding of the conductive, convective and radiative heating effects through a thermal protection system, a mathematical
 关于派博传思  派博传思旗下网站  友情链接
派博传思介绍 公司地理位置 论文服务流程 影响因子官网 SITEMAP 大讲堂 北京大学 Oxford Uni. Harvard Uni.
发展历史沿革 期刊点评 投稿经验总结 SCIENCEGARD IMPACTFACTOR 派博系数 清华大学 Yale Uni. Stanford Uni.
|Archiver|手机版|小黑屋| 派博传思国际 ( 京公网安备110108008328) GMT+8, 2025-5-4 04:51
Copyright © 2001-2015 派博传思   京公网安备110108008328 版权所有 All rights reserved
快速回复 返回顶部 返回列表