Basic Theory of Plates and Elastic Stability - Part 1
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Tài liệu tham khảo giáo trình cơ học kết cấu trong ngành xây dựng bằng Tiếng Anh - Yamaguchi, E. “Basic Theory of Plates and Elastic Stability” Structural Engineering Handbook Ed. Chen Wai-Fah Boca Raton: CRC Press LLC, 1999 - Basic Theory of Plates and Elastic Stability
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Basic Theory of Plates and Elastic Stability - Part 1Yamaguchi, E. “Basic Theory of Plates and Elastic Stability”Structural Engineering HandbookEd. Chen Wai-FahBoca Raton: CRC Press LLC, 1999 Basic Theory of Plates and Elastic Stability 1.1 Introduction 1.2 Plates Basic Assumptions • Governing Equations • Boundary Con- ditions • Circular Plate • Examples of Bending Problems 1.3 Stability Basic Concepts • Structural Instability • • Columns Thin- Walled Members • PlatesEiki Yamaguchi 1.4 Defining TermsDepartment of Civil Engineering, ReferencesKyushu Institute of Technology, Further ReadingKitakyusha, Japan1.1 IntroductionThis chapter is concerned with basic assumptions and equations of plates and basic concepts of elasticstability. Herein, we shall illustrate the concepts and the applications of these equations by means ofrelatively simple examples; more complex applications will be taken up in the following chapters.1.2 Plates1.2.1 Basic AssumptionsWe consider a continuum shown in Figure 1.1. A feature of the body is that one dimension is muchsmaller than the other two dimensions: t FIGURE 1.1: Plate. ∂w0 u(x, y, z) = u0 (x, y) − z ∂x ∂w0 ν(x, y, z) = ν0 (x, y) − z (1.4) ∂y w(x, y, z) = w0 (x, y)where u, ν, and w are displacement components in the directions of x -, y -, and z-axes, respectively.As can be realized in Equation 1.4, u0 and ν0 are displacement components associated with the planeof z = 0. Physically, Equation 1.4 implies that the linear filaments of the plate initially perpendicularto the middle surface remain straight and perpendicular to the deformed middle surface. This isknown as the Kirchhoff hypothesis. Although we have derived Equation 1.4 from Equation 1.3 in theabove, one can arrive at Equation 1.4 starting with the Kirchhoff hypothesis: the Kirchhoff hypothesisis equivalent to the assumptions of Equation 1.3.1.2.2 Governing Equations Strain-Displacement Relationships Using the strain-displacement relationships in the continuum mechanics, we can obtain thefollowing strain field associated with Equation 1.4: ∂u0 ∂ 2 w0 εx = −z ∂x ∂x 2 ∂ν0 ∂ 2 w0 εy = −z (1.5) ∂y ∂y 2 1 ∂ u0 ∂ν0 ∂ 2 w0 εxy = + −z 2 ∂y ∂x ∂x∂yThis constitutes the strain-displacement relationships for the plate theory. Equilibrium Equations In the plate theory, equilibrium conditions are considered in terms of resultant forces andmoments. This is derived by integrating the equilibrium equations over the thickness of a plate.Because of Equation 1.2, we obtain the equilibrium equations as follows: 1999 by CRC Press LLCc ∂Nxy ∂ Nx + + qx = 0 (1.6a) ∂x ∂y ∂Nxy ∂Ny + + qy = 0 (1.6b) ∂x ∂y ∂Vy ∂Vx + + qz = 0 (1.6c) ∂x ∂ywhere Nx , Ny , and Nxy are in-plane stress resultants; Vx ...
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Basic Theory of Plates and Elastic Stability - Part 1Yamaguchi, E. “Basic Theory of Plates and Elastic Stability”Structural Engineering HandbookEd. Chen Wai-FahBoca Raton: CRC Press LLC, 1999 Basic Theory of Plates and Elastic Stability 1.1 Introduction 1.2 Plates Basic Assumptions • Governing Equations • Boundary Con- ditions • Circular Plate • Examples of Bending Problems 1.3 Stability Basic Concepts • Structural Instability • • Columns Thin- Walled Members • PlatesEiki Yamaguchi 1.4 Defining TermsDepartment of Civil Engineering, ReferencesKyushu Institute of Technology, Further ReadingKitakyusha, Japan1.1 IntroductionThis chapter is concerned with basic assumptions and equations of plates and basic concepts of elasticstability. Herein, we shall illustrate the concepts and the applications of these equations by means ofrelatively simple examples; more complex applications will be taken up in the following chapters.1.2 Plates1.2.1 Basic AssumptionsWe consider a continuum shown in Figure 1.1. A feature of the body is that one dimension is muchsmaller than the other two dimensions: t FIGURE 1.1: Plate. ∂w0 u(x, y, z) = u0 (x, y) − z ∂x ∂w0 ν(x, y, z) = ν0 (x, y) − z (1.4) ∂y w(x, y, z) = w0 (x, y)where u, ν, and w are displacement components in the directions of x -, y -, and z-axes, respectively.As can be realized in Equation 1.4, u0 and ν0 are displacement components associated with the planeof z = 0. Physically, Equation 1.4 implies that the linear filaments of the plate initially perpendicularto the middle surface remain straight and perpendicular to the deformed middle surface. This isknown as the Kirchhoff hypothesis. Although we have derived Equation 1.4 from Equation 1.3 in theabove, one can arrive at Equation 1.4 starting with the Kirchhoff hypothesis: the Kirchhoff hypothesisis equivalent to the assumptions of Equation 1.3.1.2.2 Governing Equations Strain-Displacement Relationships Using the strain-displacement relationships in the continuum mechanics, we can obtain thefollowing strain field associated with Equation 1.4: ∂u0 ∂ 2 w0 εx = −z ∂x ∂x 2 ∂ν0 ∂ 2 w0 εy = −z (1.5) ∂y ∂y 2 1 ∂ u0 ∂ν0 ∂ 2 w0 εxy = + −z 2 ∂y ∂x ∂x∂yThis constitutes the strain-displacement relationships for the plate theory. Equilibrium Equations In the plate theory, equilibrium conditions are considered in terms of resultant forces andmoments. This is derived by integrating the equilibrium equations over the thickness of a plate.Because of Equation 1.2, we obtain the equilibrium equations as follows: 1999 by CRC Press LLCc ∂Nxy ∂ Nx + + qx = 0 (1.6a) ∂x ∂y ∂Nxy ∂Ny + + qy = 0 (1.6b) ∂x ∂y ∂Vy ∂Vx + + qz = 0 (1.6c) ∂x ∂ywhere Nx , Ny , and Nxy are in-plane stress resultants; Vx ...
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