Tables 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
  • Table 1. Design Values for Low Modulus (LM) Graphite-Epoxy Composite
  • Table 2. Design Values for High Modulus (HM) Graphite-Epoxy Composite
  • Table 3. Design Values for Ultra Modulus (UM) Graphite-Epoxy Composite
  • Table 4. Aircraft and Visualize Wing Loads Parameters
  • Table 5. Results of the Various Graphite_Epoxy Spar Designs