• Shuffle
Toggle On
Toggle Off
• Alphabetize
Toggle On
Toggle Off
• Front First
Toggle On
Toggle Off
• Both Sides
Toggle On
Toggle Off
Toggle On
Toggle Off
Front

### How to study your flashcards.

Right/Left arrow keys: Navigate between flashcards.right arrow keyleft arrow key

Up/Down arrow keys: Flip the card between the front and back.down keyup key

H key: Show hint (3rd side).h key

A key: Read text to speech.a key

Play button

Play button

Progress

1/14

Click to flip

### 14 Cards in this Set

• Front
• Back
 is a state of balance or zero motion Equilibrium is a simplified sketch of a structure or part of a structure solated from its supports which shows all active and reactive forces acting on the structure Free Body Diagram Are structural members that resist loads applied transverse to their longitudinal axis Beams two bracing systems that provide lateral stability for a pinned frame Rigid Frame and Shearwalls Roof and floors are horiontal planes that must be supported against lateral movement. these horizontal planes are called Diaphragms Lateral force-resisting walls are called Shearwalls Loads uniformly distrobuted over and area of a roof or floor are assigned to individual members based on the concept of Transverse shear force is the manner in which loads travel throughout thhe structure load path involves the sysematic prcess of determining loads and support reactions of individual structural members as they in turn affect the loading of other structural elements load tracing is a tranverse section in a beam span where the bending momnet is zero point of inflection the sagging of a beam subjected to loads that create bending deflection the equations of static equilibrium for a rigid body that lies on a plane (x,y) Sum Fy = 0 Sum Fx = 0 Sum M = 0 the internal force system, which exists within a beam to resist the applied forces and moments, consists of The bending Moment, Shear, and Normal Force equation that indicates that at any section in the beam the slope of the moment diagram is equal to the shear. dm/dx = V