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Non-Metal Composite
I-Beam (Carbon-Fiber)
ALDEN ST.MARY, JACK WALKER, KUNIND SHARMA
Article Summary
 CPSU students created a carbon fiber composite I-beam for a bridge
support competition.
 Carbon Fiber can be created through winding, laying, and molding.
 Different Curing temperatures and times can produce CF with varying
mechanical properties to suit the design conditions.
 Carbon Fiber was chosen due to its extreme strength and stiffness versus
other materials, especially in an I-beam configuration.
 The Molding Method was used to create the I-beam as it is conducive to
high strength under compression and tension.
 The Final Product weighed only 600 grams and could support a 3000 lb
load.
Material properties of Carbon Fiber
 Several highly favorable mechanical properties
 Excellent Strength to weight ratio (50 times that of cold rolled steel)
 Low Density (1.75 g/cm^3)
 Very High Tensile Strength- greater than 4000 MPa and up to 6000 MPa in some cases
 Corrosion Resistant and Chemically Stable
 Electrically Conductive
 High Stiffness and Toughness
 High Modulus of Elasticity (100 to 140 GPa)
 High In-plane Shear Strength – 90 MPa
 Very Brittle – Failure occurs violently and with little to no signs of deformation before
fracture
 Little to no Ductility – result of hexagonal nanotube microstructure
FBD of Loaded Beam
y
x
Cross Sectional and Calculations
Shear and Moment Diagrams
65.5205
64.472
Max. Bending moment
74.005
Moment
goes to 0
Moment
goes to 0
Max. Shear9.263
Shear goes to 0
Mohr’s Circle Equations
 Axial Stress: sx = M y/I = 74.005(kip/in)* (2in)/(8.47in4)= 17.47 (kip/in2)
 Shear Stress: txy= sx /2= (17.47)/2 = 8.737 (kip/in2)
 sy= [2(txy/tan(2θp))] – sx= [2(8.737/tan(60))] – 17.47= 7.38(kip/in2)
 Avg. Stress (Center) = (sx+sy)/2= (17.47+7.38)/2= 12.425(kip/in2)
 Maximum Shear Stress (Radius)= 𝑐𝑒𝑛𝑡𝑒𝑟 − sy
2 + txy
2
= 12.425 − 7.38 2 + 76.3352 = R=10.09
Mohr’s Circle
Principal Stresses Maximum Shear Stresses
Original Stresses
Principal Stresses
Shear Stresses
References
 Rider, Kodi, Nino Noel Las Pinas, and Hans Mayta. Composite I - Beam
Fabrication and Testing in Response to 14 Th Annual SAMPE Bridge
Competition. Calpoly.edu. N.p., 9 June 2011. Web.
<http://digitalcommons.calpoly.edu/cgi/viewcontent.cgi?article=1046&co
ntext=aerosp>.
 "MecMovies - Mechanics of Materials." MecMovies - Mechanics of
Materials. N.p., n.d. Web. 02 Dec. 2015.
<http://web.mst.edu/~mecmovie/>.
 "Mechanical Properties of Carbon Fibre Composite Materials, Fibre / Epoxy
Resin (120°C Cure)." Mechanical Properties of Carbon Fibre Composite
Materials. N.p., n.d. Web. 02 Dec. 2015. <http://www.performance-
composites.com/carbonfibre/mechanicalproperties_2.asp>.

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Non-Metal (Composite) I-Beam

  • 1. Non-Metal Composite I-Beam (Carbon-Fiber) ALDEN ST.MARY, JACK WALKER, KUNIND SHARMA
  • 2. Article Summary  CPSU students created a carbon fiber composite I-beam for a bridge support competition.  Carbon Fiber can be created through winding, laying, and molding.  Different Curing temperatures and times can produce CF with varying mechanical properties to suit the design conditions.  Carbon Fiber was chosen due to its extreme strength and stiffness versus other materials, especially in an I-beam configuration.  The Molding Method was used to create the I-beam as it is conducive to high strength under compression and tension.  The Final Product weighed only 600 grams and could support a 3000 lb load.
  • 3. Material properties of Carbon Fiber  Several highly favorable mechanical properties  Excellent Strength to weight ratio (50 times that of cold rolled steel)  Low Density (1.75 g/cm^3)  Very High Tensile Strength- greater than 4000 MPa and up to 6000 MPa in some cases  Corrosion Resistant and Chemically Stable  Electrically Conductive  High Stiffness and Toughness  High Modulus of Elasticity (100 to 140 GPa)  High In-plane Shear Strength – 90 MPa  Very Brittle – Failure occurs violently and with little to no signs of deformation before fracture  Little to no Ductility – result of hexagonal nanotube microstructure
  • 4. FBD of Loaded Beam y x
  • 5. Cross Sectional and Calculations
  • 6. Shear and Moment Diagrams 65.5205 64.472 Max. Bending moment 74.005 Moment goes to 0 Moment goes to 0 Max. Shear9.263 Shear goes to 0
  • 7. Mohr’s Circle Equations  Axial Stress: sx = M y/I = 74.005(kip/in)* (2in)/(8.47in4)= 17.47 (kip/in2)  Shear Stress: txy= sx /2= (17.47)/2 = 8.737 (kip/in2)  sy= [2(txy/tan(2θp))] – sx= [2(8.737/tan(60))] – 17.47= 7.38(kip/in2)  Avg. Stress (Center) = (sx+sy)/2= (17.47+7.38)/2= 12.425(kip/in2)  Maximum Shear Stress (Radius)= 𝑐𝑒𝑛𝑡𝑒𝑟 − sy 2 + txy 2 = 12.425 − 7.38 2 + 76.3352 = R=10.09
  • 8. Mohr’s Circle Principal Stresses Maximum Shear Stresses Original Stresses Principal Stresses Shear Stresses
  • 9. References  Rider, Kodi, Nino Noel Las Pinas, and Hans Mayta. Composite I - Beam Fabrication and Testing in Response to 14 Th Annual SAMPE Bridge Competition. Calpoly.edu. N.p., 9 June 2011. Web. <http://digitalcommons.calpoly.edu/cgi/viewcontent.cgi?article=1046&co ntext=aerosp>.  "MecMovies - Mechanics of Materials." MecMovies - Mechanics of Materials. N.p., n.d. Web. 02 Dec. 2015. <http://web.mst.edu/~mecmovie/>.  "Mechanical Properties of Carbon Fibre Composite Materials, Fibre / Epoxy Resin (120°C Cure)." Mechanical Properties of Carbon Fibre Composite Materials. N.p., n.d. Web. 02 Dec. 2015. <http://www.performance- composites.com/carbonfibre/mechanicalproperties_2.asp>.