Figures index

From

Graphite-epoxy Composite Design for Aircrcaft Wing Spar Using Computational Techniques – Part I

AKINDAPO Jacob Olaitan, JOHNSON-ANAMEMENA Nnaemeka, GARBA Danladi King

American Journal of Mechanical Engineering. 2017, 5(4), 117-127 doi:10.12691/ajme-5-4-2
  • Figure 1. Lift on the wing
  • Figure 2. Load due to wing structure weight
  • Figure 3. Load due to the weight of the fuel stored in the wing
  • Figure 4. Airfoil Terminology (Source: Dynamic Flight Inc. [4])
  • Figure 5. Primary Variables of Airfoil (Source: Jeff Scott [6])
  • Figure 6. MATLAB generated plot for the various load components along the length of the aircraft wing
  • Figure 7. MATLAB generated plot for shear force
  • Figure 8. MATLAB generated plot for bending moment along the length of the aircraft wing.
  • Figure 9. Section Preview of LM Graphite_Epoxy Spar
  • Figure 10. Deflection of LM Graphite_Epoxy Spar
  • Figure 11. Nodal Solution of Deflected LM Graphite_Epoxy Spar
  • Figure 12. Von Mises Stress of LM Graphite_Epoxy Spar
  • Figure 13. XY Shear Stress of LM Graphite_Epoxy Spar
  • Figure 14. Section Preview of HM Graphite_Epoxy Spar
  • Figure 15. Deflection of HM Graphite_Epoxy Spar
  • Figure 16. Nodal Solution of Deflected HM Graphite_Epoxy Spar
  • Figure 17. von Mises Stress of HM Graphite_Epoxy Spar
  • Figure 18. XY Shear Stress of HM Graphite_Epoxy Spar
  • Figure 19. Section Preview of UM Graphite_Epoxy Spar
  • Figure 20. Deflection of UM Graphite_Epoxy Spar
  • Figure 21. Nodal Solution of Deflected UM Graphite_Epoxy Spar
  • Figure 22. Von Mises Stress of UM Graphite_Epoxy Spar
  • Figure 23. XY Shear Stress of UM Graphite_Epoxy Spar