3.3 Principal structural elements in an aircraft


Axial members carry extensional and compressive loads

Pinned column (axial member, i.e. a strut) Wikipedia, Dammit, 2007, CCSA2.5 AgnosticPreachersKid, Wikipedia, 2008 CCSA3.0

Also called columns


Bending members carry bending moments

https://bh-usa.com/wp-content/uploads/2017/09/6061-Aluminum-I-Beam-2.jpg Adrian Pingstone, 2008, Public Domain Cantilever beam (bending member, i.e. wing)

  • A subset of bending members are called beams

Torsion members carry twisting moments (torques)

Shaft (torsion member) Jeff Dean, 2007, CCSA

  • A subset can be called shafts (but not all torsion members should be called shafts)
    • i.e., Crankshafts
  • Other structural members carry torsion
    • fuselages
    • wings

Shear panel

  • A thin sheet of material used to carry in-plane shear load
  • Skin (shear member, i.e wing panel)

Beam on an elastic foundation

https://www.researchgate.net/figure/285530512_fig2_Figure-2-Beam-resting-on-two-parameter-elastic-foundation Sean Lambo, 2004, CCSA2.0


Membrane


Plates and shells

gwultrasonics.com dianafea.com


Curved beams


Combinations

Optimal aerostructures typically combine several structural features:

Original Source Unknown – Multiple Sources


Load Paths

Wing skins \(\Longrightarrow\) stringers \(\Longrightarrow\) ribs \(\Longrightarrow\) spars \(\Longrightarrow\) fuselage

@Sun2006 Figure 1.9 @Sun2006 Figure 1.10 @Sun2006 Figure 1.12 @Sun2006 Figure 1.14


787 Fuselage (Composite Construction)