Introduction to Aircraft Structural Analysis (Elsevier Aerospace Engineering)

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78 CHAPTER 3 Torsion of Solid Sections


Fig.3.7


Membrane analogy: in-plane and transverse loading.


Fig.3.8


Equilibrium of element of membrane.


Equation(3.24)mustbesatisfiedatallpointswithintheboundaryofthemembrane.Furthermore,
atallpointsontheboundary


w= 0 (3.25)

andweseethatbycomparingEqs.(3.24)and(3.25)withEqs.(3.11)and(3.7),wisanalogoustoφ
whenqisconstant.Thus,ifthemembranehasthesameexternalshapeasthecrosssectionofthebar,
then


w(x,y)=φ(x,y)
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