Basics of Structural Analysis: Difference between revisions
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* Shearing force <math>\frac{V(x)}{x} = -w(x) </math>. Thus we have <math>\Delta V =\int w(x) dx </math>. <math>w(x)</math> is the intensity of applied (normal?) force. | * Shearing force <math>\frac{V(x)}{x} = -w(x) </math>. Thus we have <math>\Delta V =\int w(x) dx </math>. <math>w(x)</math> is the intensity of applied (normal?) force. | ||
* Bending moment <math>\frac{dM}{dx} = V(x)</Math> and thus <math>\frac{d^2M}{dx^2} = -w(x)</Math>. | * Bending moment <math>\frac{dM}{dx} = V(x)</Math> and thus <math>\frac{d^2M}{dx^2} = -w(x)</Math>. | ||
=== Deflection of beams === | |||
The strain <math>\epsilon</math> in the filament is due to the different lengths of filaments in bended beam. <math>\epsilon = </math> | |||
== Column == | == Column == |
Revision as of 11:21, 20 January 2024
Introduction
Structural analysis using about high school level physics and maths.
Aim to calculate fiberglass cansat structure
Basic theory
Principle of superposition: linearity. Displacement at location from forces and </math>P_2</math> located at different positions is calculated as
The energy principle: giving the total energy as which is called strain energy. For linear deformation this gives .
Virtual work principle.
Dead loads, live loads, impact loads (impact factor), wind loads.
Equilibrium.
Forces:
- Normal force and axial force
- Shearing force . Thus we have . is the intensity of applied (normal?) force.
- Bending moment and thus .
Plate
Beam
Forces:
- Normal force and axial force
- Shearing force . Thus we have . is the intensity of applied (normal?) force.
- Bending moment and thus .
Deflection of beams
The strain in the filament is due to the different lengths of filaments in bended beam.
Column
Column is a vertical beam.