Page 606 - Aircraft Stuctures for Engineering Student
P. 606

Index  587

               principal curvatures 127            Sandwich panels 230,23 1
               principal moments 127               Secant modulus 173
               pure bending 122-5                  Second moments of area of inclined and
               secant modulus 173                   curved thin sections 288,289
               strain energy in bending and twisting 142,   Semi-inverse method for elasticity problems
                 143                                41,43-8
               subjected to a distributed transverse load   Semi-monocoque structures 223
                 129-37                            Shear centre 295,298-300,  304-7,  392
               synclastic surface 125              Shear lag, see Structural constraint
               tangent modulus 173                 Shear lines 57
               total potential energy 147          Shear of closed section beams 300-7
              Poisson's ratio 25                     alternative method for the calculation of
               limiting value 26                      shear flow distribution 340, 341
              Polar second moment of area of a thin-   shear centre 304-7
               walled column 184                     shear flow distribution 300-2
              Potential energy 70, 71, 73-6,  144-9,  165-9   twist and warping 303,304
              Prandtl stress function, see Torsion of solid   Shear of fuselages, see Stress analysis of
               sections                              aircraft components
              Principal axes of a beam section 81   Shear of open section beams 295-300
              Principal planes 11                    alternative method for the calculation of
              Principal strains 23                    shear flow distribution 340, 341
              Principal stresses 11, 12              shear centre 298-300
              Principle of stationary value of total   shear flow distribution 295-8
               complementary energy 76, 77         Shear of wings, see Stress analysis of aircraft
               application to deflection problems 77-85   components
               application to statically indeterminate   Shear stress distribution at a built-in end of
                 systems 85-100                      a closed section beam 445-8
              Principle of stationary value of total   Slenderness ratio of a column, see Columns
               potential energy 73-6,  142-9       Southwell plot
              Principle of superposition 103         columns 162
              Principle of virtual work 71-3         plates 174
               virtual displacements 7 1, 72       Stability of beams under transverse and
               virtual forces 72, 73                 axial loads 162-5
              Principles of stressed skin construction   Stainless steel, see Materials of aircraft
                21 1-32                              construction
                                                   Statically determinate systems 24
              Rayleigh, Lord 103, 565              Statically indeterminate systems 24, 85-100
              Rayleigh-Ritz  method                Stiffened panels 175-80
                bending of a beam 75                 failure stress 177-80
                buckling of columns 168              instability 175-7
                oscillation of beams 565-8         Strain 16-32
                thin plates 142-9                    definition 17
              Reciprocal theorem 68                  experimental measurement 28-32
              Reduced elastic modulus of a column 159   longitudinal or direct strain 16- 18
                                                     maximum shear strain 23
              Safe life structures, see Fatigue      Mohr's  circle 23, 28
              St. Venant, B. de                      plane strain 20, 37, 38
                principle 42                         principal strains 23
                semi-inverse method 41, 43-8         shear strain 16, 18, 19
                warping function, see Torsion of solid   strain gauge rosette 29
                 sections                            strains on inclined planes 21, 22
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