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一、飞机 二、飞机设计 三、飞机设计阶段 (1)拟定飞机设计要求 (2)概念设计(决策点1,军委+国务院,设计要求) (3)初步设计 (4)详细设计(决策点2,总参+科工委,样机) (5)原型机试制 (6)试飞(决策点3,军委+国务院,原型机) (7)成批生产(决策点4,总参+科工委,生产型飞机) (8)使用和改进改型
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3.1设计的任务和步骤 3.1.1飞机总体参数详细设计的最优化准则设计的主要任务是保证飞机总体参数的最优化
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5.1飞机寿命周期费用的概念和分析方法 5.1.1飞机寿命周期费用的提出 5.1.2寿命和寿命周期费用的基本概念 1、飞机的寿命(life) 飞机的寿命是从人的寿命这一概念借用来的,用来表示飞机的 耐久性。一般来说,有关飞机寿命的概念主要有两种:自然寿命和 规定寿命
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16.21 Techniques of Structural Analysis and sig Spring 2003 Unit #1 In this course we are going to focus on energy and variational methods for structural analysis. To understand the overall approach we start by con- trasting it with the alternative vector mechanics approach
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We are going to consider the forces exerted on a material. These can be external or internal. External forces come in two flavors: body forces(given per unit mass or volume) and surface forces(given per unit area). If we cut a body of material in equilibrium under a set of external forces along a plane as shown in fig. 1. and consider one side of it we draw two conclusions: 1 the equilibrium provided by the loads from the side taken out is provided by a set of forces that are distributed among the material particles adjacent to
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A Cauchy stress component at a given(fixed) point P of a structure in equilibrium under the action of external loads is defined when 1. the direction of the face on which the stress component acts is specified 2 the direction of the force from which the stress component is derived is specified None of the above statements
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The following expression is the right statement of linear momentum balance for a deforming body of an arbitrary material
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We seek to characterize the local state of deformation of the material in a neighborhood of a point P. Consider two points P and Q in the undeformed
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For the uniform state of plane strain shown in the fig ure,which one(s) of the following statement(s) is(are valid?(Assume Poisson's ratio v+0)
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The following stress-strain curves were obtained for dif- ferent materials subjecting the specimen to the loading path(a, b, c, d ). Which one(s) of them correspond to elas- tic material(s)
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