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

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樓主: bile-acids
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發(fā)表于 2025-3-28 15:40:44 | 只看該作者
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發(fā)表于 2025-3-29 00:13:18 | 只看該作者
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
44#
發(fā)表于 2025-3-29 05:08:06 | 只看該作者
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
45#
發(fā)表于 2025-3-29 07:17:45 | 只看該作者
46#
發(fā)表于 2025-3-29 14:34:23 | 只看該作者
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
47#
發(fā)表于 2025-3-29 19:31:53 | 只看該作者
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
48#
發(fā)表于 2025-3-29 21:06:39 | 只看該作者
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
49#
發(fā)表于 2025-3-30 01:36:26 | 只看該作者
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
50#
發(fā)表于 2025-3-30 04:41:13 | 只看該作者
,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
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