Structural Mechanics Flashcards
Structural redundancy/ Indeterminancy number (α) ?
The number of extra unknowns in relation to a statically determinate system
Redundancy formula?
External (de) + internal (ai) redundancy
How do hinges affect redundancy?
-1 redundancy for each internal hinge because it adds an equation
What redundancy do local mechanisms have?
Local mechanisms can appear >_ 0 total redundancy
How do cells affect redundancy?
+3* number of cells to redundancy
How do bars in trusses that connect to existing nodes effect redundancy?
In a truss add redundancy for each extra bar connecting two existing nodes in a truss minus the number of internal hinges
d1(U)=Δd(W)
Virtual internal forces* real deformations = virtual external forces* real displacements
How to work out displacements for trusses?
Sum of all virtual axis forces (N) x Real strains (ε) = 1* real displacement
How to work out displacements for beams and frames?
Sum of all virtual bending moments (M) * Real curvatures(k) = 1 x real displacement
Structure (SIS) = +*_
Structure (SIS) = Case 0 (SDS) + X1 (unknown) * Case 1 (SDS)
Flexibility method of statically indeterminate structures ( removing supports)?
- Obtain the redundancy
- Identify α supports that can be removed maintaining equilibrium
- Replace the supports by the unknown reactions
- Decompound the initial structure in α+1 load cases. Apply the external loads in Case 0, and the reactions equal to 1 times the unknowns for the other α cases
- Obtain the vertical displacements at the supports that have been removed (using the unit load method, with unit loads equal to the load cases 1 to α, and applying superposition)
- Impose the compatibility equation displacement = 0 at each removed support and obtain the unkowns
Flexibility method for statically indeterminate structures (adding hinges)?
- Obtain the redundancy
- Identify α hinges that can be added maintaining equilibrium
- Replace each continuous section by a hinge and the corresponding unknown bending moment (couple of moments)
- Decompound the initial structure in α+1 load cases. Apply the external loads in case 0, an a couple of unityoments times the unknowns for the other α cases
- Obtain the angular dislocations at the hinges (using the unit load method, with unit loads equal to the load cases 1 to α, and applying superposition)
- Impose the compatibility equation dislocation=0 at each added hinge , and obtain unkowns
F1= Σ ((N0 L)/(EA) + ΔL0) N1
N0= axial forces in case 0 (real)
EA= youngs modulus*area
L= length of beam
ΔL = change in length
N1= axial force in case 1
F1= unknown force
F2= Σ ((N1)^2* L)/EA
E= Young’s modulus
A= area
N1= Axial force of case 1
L= length of beam
F1 + F2 * X1 = 0
X1= unknown force
What is the product integral of two rectangles?
Lab
Length* height of one rectangle * height of second rectangle
What is the product integral of a triangle and rectangle?
1/2 * L * a * b
L= length
a= height of triangle
b= height of rectangle
What is the product integral of two triangles?
1/3 * L * a * b
L= length
a= height of triangle one
b= height of triangle two
What is the product integral of two triangles in opposite directions?
1/6 L a b
Length * height of one triangle * height of two triangle
What is the product integral of a not right angled triangle and a right angle triangle ?
1/4 Lab
L= length
a= height of one triangle
b= height of second triangle
What is the product integral of a rectangle and semi circle?
2/3 Lab
Length* height of rectangle * radius