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ANALYSIS OF TRUSS
Syed Raheel Zafar
WHAT IS TRUSS?
• A truss is a structure comprising one or more
triangular units constructed with straight
members whose ends are connected at joints.
• If all the bars lie in a plane, the structure is a
planar truss.
• The main parts of a planar truss.
ANALYSIS OF FRAME
• A FRAME IS A STRUCTURE MADE OF SEVERAL BARS/ RODS
WELDED / RIVETTED TOGETHER
• THE BARS ARE ANGLE IRONS/ CHANNELS OF “I” OR “T”
SECTIONS. THESE ARE CALLED MEMBERS
• ON APPLICATION OF LOAD ON TO THE STRUCTURE, THE
MEMBERS REMAIN LOADED WITH TENSILE/ COMPRESSIVE
LOAD
• MEMBERS UNDER TENSION
• MEMBERS UNDER COMPRESSION
• THE STRUCTURE FORMED BY THE MEMBERS IS CALLED
“TRUSS”
• EXTENSIVELY USED IN ROOF, BRIDGE, SHEDS ETC.
STRESSES IN A FRAME
• UNDER APPLICATION OF LOAD THE STRUCTURE
TENDS TO DEFORM. THE MATERIAL OF THE FRAME
TENDS TO KEEP THE FRAME RIGID ( PREVENTS
DEFORMATION)
• AN INTERNAL RESISTIVE FORCE IS SET IN IN THE
MATERIAL . THIS INDUCES STRESS.
• σ = INTERNAL RESISTANCE / AREA
• LOAD CAN BE PULL / PUSH (TENSILE/ COMPRESSIVE)
• FOR JOINTS TO BE IN EQUILIBRIUM THE MEMBERS
MAY CARRY ZERO LOAD/ TENSILE/ COMPRESSIVE
LOAD.
CONVENTIONS
• ANALYST HAS TO IDENTIFY THE SITUATION ,
MAKE A MENTAL PICTURE OF THE FORCES
AND DECIDE THE ARROWS.
• A LOAD WITH ARROW AWAY FROM THE
JOINT IS TENSILE
• A LOAD WITH ARROW TOWARDS THE JOINT
IS COMPRESSIVE
ASSUMPTIONS
MEMBERS ARE RIGIDILY JOINT (Every member
of the truss is then in pure compression or pure
tension – shear, bending moment, and other
more complex stresses are all practically zero. )
•LOADS ACT ON THE JOINTS ONLY
•WEIGHT OF THE MEMBER AS COMPARED TO
THE EXTERNAL LOADS IS NEGLIGIBLE AND NOT
CONSIDERED FOR CALCULATIONS.
SOLUTIONS
ANALYTICAL
• USE OF TRIGONOMETRY/
GEOMETRY/ ALGEBRA
• TWO METHODS (JOINT &
SECTION METHODS)
• THE METHODS CAN BE
CUMBERSOME AND LENGTHY
AND LEAD TO ERRORS
• A COMPARISON ON NEXT
SLIDE
GRAPHICAL
• USE OF CONCEPT OF ENGG DRG
• USE OF SPACE, VECTOR DIAGRAM
AND A LOAD TABLE
• VECTOR DIAGRAM OF EACH JOINT
(MAXWELL DIAGRAM) AND
COMPOSITE VECTOR DIAGRAM
GIVES THE SOLUTION
• SELECT THE 1ST
JOINT WITH 2 UNK
FORCES AND THEN PROCEED TO THE
NEXT JOINT
• IT IS SIMPLE , EASY AND FULL PROOF
• INITALLY ANALYTICAL METOD TOBE
USED FOR CALCULATION OF
REACTIONS
ANALYTICAL SOLUTIONS
JOINT METHOD
• FORCES OF EA JOINT IS ANALYSID
ONE BY ONE
• SELECT A JOINT WITH 2 UNK
FORCES
• ANALYSE THE FORCES AT THAT
JOINT MATHEMATEICALLY AND
THEN PROCEED TO THE NEXT
• FOR COMPLEX FRAME THIS
METHOD IS VERY LONG AND CAN
LEAD TO MATHEMATICAL ERRORS
SECTION METHOD
• THE FRAME IS CUT INTO
SECTIONS
• EA SECTION IS THEREAFTER
ANALYSED USING FBD
• MOMENTS OF EACH MEMBER
W.R.T. A REF POINT IS
CALCULATED AND THE
FORCES ARE BVDETERMINED
• SECTION LINE MUST NOT CUT
MORE THAN 3 MEMBERS
• IT IS VERY TEDIOUS FOR
COMPLEX STRUCTURES
LEARNING OUTCOME
• Types of joints and supports
• Zero force members
• Material choice
• Factor of safety
• Design analysis
• Trial and error

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Analysis of Truss

  • 3. WHAT IS TRUSS? • A truss is a structure comprising one or more triangular units constructed with straight members whose ends are connected at joints. • If all the bars lie in a plane, the structure is a planar truss. • The main parts of a planar truss.
  • 4. ANALYSIS OF FRAME • A FRAME IS A STRUCTURE MADE OF SEVERAL BARS/ RODS WELDED / RIVETTED TOGETHER • THE BARS ARE ANGLE IRONS/ CHANNELS OF “I” OR “T” SECTIONS. THESE ARE CALLED MEMBERS • ON APPLICATION OF LOAD ON TO THE STRUCTURE, THE MEMBERS REMAIN LOADED WITH TENSILE/ COMPRESSIVE LOAD • MEMBERS UNDER TENSION • MEMBERS UNDER COMPRESSION • THE STRUCTURE FORMED BY THE MEMBERS IS CALLED “TRUSS” • EXTENSIVELY USED IN ROOF, BRIDGE, SHEDS ETC.
  • 5. STRESSES IN A FRAME • UNDER APPLICATION OF LOAD THE STRUCTURE TENDS TO DEFORM. THE MATERIAL OF THE FRAME TENDS TO KEEP THE FRAME RIGID ( PREVENTS DEFORMATION) • AN INTERNAL RESISTIVE FORCE IS SET IN IN THE MATERIAL . THIS INDUCES STRESS. • σ = INTERNAL RESISTANCE / AREA • LOAD CAN BE PULL / PUSH (TENSILE/ COMPRESSIVE) • FOR JOINTS TO BE IN EQUILIBRIUM THE MEMBERS MAY CARRY ZERO LOAD/ TENSILE/ COMPRESSIVE LOAD.
  • 6. CONVENTIONS • ANALYST HAS TO IDENTIFY THE SITUATION , MAKE A MENTAL PICTURE OF THE FORCES AND DECIDE THE ARROWS. • A LOAD WITH ARROW AWAY FROM THE JOINT IS TENSILE • A LOAD WITH ARROW TOWARDS THE JOINT IS COMPRESSIVE
  • 7. ASSUMPTIONS MEMBERS ARE RIGIDILY JOINT (Every member of the truss is then in pure compression or pure tension – shear, bending moment, and other more complex stresses are all practically zero. ) •LOADS ACT ON THE JOINTS ONLY •WEIGHT OF THE MEMBER AS COMPARED TO THE EXTERNAL LOADS IS NEGLIGIBLE AND NOT CONSIDERED FOR CALCULATIONS.
  • 8. SOLUTIONS ANALYTICAL • USE OF TRIGONOMETRY/ GEOMETRY/ ALGEBRA • TWO METHODS (JOINT & SECTION METHODS) • THE METHODS CAN BE CUMBERSOME AND LENGTHY AND LEAD TO ERRORS • A COMPARISON ON NEXT SLIDE GRAPHICAL • USE OF CONCEPT OF ENGG DRG • USE OF SPACE, VECTOR DIAGRAM AND A LOAD TABLE • VECTOR DIAGRAM OF EACH JOINT (MAXWELL DIAGRAM) AND COMPOSITE VECTOR DIAGRAM GIVES THE SOLUTION • SELECT THE 1ST JOINT WITH 2 UNK FORCES AND THEN PROCEED TO THE NEXT JOINT • IT IS SIMPLE , EASY AND FULL PROOF • INITALLY ANALYTICAL METOD TOBE USED FOR CALCULATION OF REACTIONS
  • 9. ANALYTICAL SOLUTIONS JOINT METHOD • FORCES OF EA JOINT IS ANALYSID ONE BY ONE • SELECT A JOINT WITH 2 UNK FORCES • ANALYSE THE FORCES AT THAT JOINT MATHEMATEICALLY AND THEN PROCEED TO THE NEXT • FOR COMPLEX FRAME THIS METHOD IS VERY LONG AND CAN LEAD TO MATHEMATICAL ERRORS SECTION METHOD • THE FRAME IS CUT INTO SECTIONS • EA SECTION IS THEREAFTER ANALYSED USING FBD • MOMENTS OF EACH MEMBER W.R.T. A REF POINT IS CALCULATED AND THE FORCES ARE BVDETERMINED • SECTION LINE MUST NOT CUT MORE THAN 3 MEMBERS • IT IS VERY TEDIOUS FOR COMPLEX STRUCTURES
  • 10. LEARNING OUTCOME • Types of joints and supports • Zero force members • Material choice • Factor of safety • Design analysis • Trial and error