Page 462 - Aircraft Stuctures for Engineering Student
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Structural constraint











          The analysis presented in Chapters 9 and 10 relies on elementary theory for the deter-
          mination  of  stresses and  displacements produced  by  axial loads,  shear  forces and
          bending moments and torsion. Thus, no allowance is made for the effects of restrained
          warping produced by  structural or loading discontinuities in the torsion of open or
          closed section beams, or for the effects of  shear strains on the calculation of direct
          and shear stresses in beams subjected to bending and shear.
            In  this  chapter we  shall examine some relatively  simple examples of  the  above
          effects; more complex cases require analysis by computer-based  techniques such as
          the finite element method.






          Structural constraint stresses in either closed or open beams result from a restriction
          on the  freedom of  any section of  the  beam to assume its normal  displaced shape
          under load. Such a restriction arises when one end of the beam is built-in although
          the same effect may  be  produced  practically, in a variety of ways. Thus, the  root
          section of a beam subjected to torsion  is completely restrained  from warping into
          the displaced shape indicated by Eq. (9.52) and a longitudinal stress system is induced
          which, in  a  special case discussed later, is proportional  to the free warping of  the
          beam.
            A slightly different situation arises when the beam supports shear loads. The stress
          system predicted  by  elementary bending  theory  relies on the  basic  assumption  of
          plane sections remaining plane after bending. However, for a box beam comprising
          thin skins and booms,  the shear strains in  the skins are of  sufficient magnitude  to
          cause a measurable redistribution  of direct load in the booms and hence previously
          plane sections warp. We shall discuss the phenomenon of load redistribution resulting
          from shear, known as shear lag, in detail later in the chapter. The prevention of this
          warping by some form of axial constraint modifies the stress system still further.
            The most  comprehensive analysis yet published  of multi- and  single cell  beams
          under  arbitrary  loading  and  support  conditions  is  that  by  Argyris  and  Dunne'.
          Their work concentrates in the main on beams of idealized cross-section and while
          the theory they present is in advance of that required here, it is beneficial to examine
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