Page 604 - Aircraft Stuctures for Engineering Student
P. 604

index  585

              Finite-element method, see Matrix methods   Gust loads, see Airworthiness
              Flexibility coefficient 103
              Flexural axis 444                    Hiduminium RR58 215,216
              Flexural rigidity                    Homogeneous materials 24
                of a beam 82                       Hooke’s law 24
                of a plate 124
              Flexural-torsional buckling of thin-walled   Inelastic buckling of columns, see Columns
                columns 180-8                      Inelastic buckling of plates 173
              Flight envelope, see Airworthiness     plasticity correction factor 173
              Flutter 540, 568-76                    secant modulus 173
                aileron buzz 570                     tangent modulus 173
                buffeting 570                      Inertia loads aircraft 238-43
                classical flutter 570              Influence coefficient, see Flexibility
                control surface flutter 575, 576     coefficient
                  ground resonance test 576        Instability of stiffened panels 175-7
                  mass balancing 576               Integral construction 230
                coupling 570-2                     Interrivet buckling in stiffened panels 177
                  aerodynamic 571                  Inverse method for elasticity problems
                  centre of independence 571         39-42
                  elastic 571, 572                 Isotropic materials 24
                  inertial 570
                determination of critical flutter speed   Kevlar 218
                  572-4                            Kirchhoff, G.R. 133
                experimental determination of flutter
                  speed 575                        Laminated composite structures, see Stress
                prevention 574-5                     analysis of aircraft components
                stalling flutter 570               Laplacian operator 53, 131
                wing bending-torsion flutter 569   Law of mixtures 426
              Force 4                              Limit load, see Airworthiness
                body forces 7                      Load factors, see Airworthiness
                internal at a point 4              Load intensity, shear force and bending
                internal components 4                moment relationships 283, 284
                notation 5-7                       Loads on structural components 220-3
                surface forces 7                     aerodynamic forces 221-3
              Fourier series for plate deflection 135   aerodynamic centre 221
              Function of structural components 223-5   centre of pressure 221
                fuselage components 225                drag 221
                nionocoque structures 223              lift 221, 222
                semi-monocoque structures 223          pitching moment 221
                tail unit 225                          yawing moment 221
                wing components 223-5                air loads 220
              Fuselage components 225                body forces 220
              Fuselages, analysis, see Stress analysis of   ground loads 220
                aircraft components                  surface forces 220
              Fuselage frames and wing ribs, see Stress   see also Airworthiness; Fatigue
                analysis of aircraft components    Local instability of thin-walled columns
                                                     174, 175
              Glass, see Materials of aircraft construction   Lumped mass concept 552
              Glass reinforced plastic 218, 219
              Goodman diagram 261                  Maraging steels 216
              Ground resonance tests, see Flutter   Mass balancing, see Flutter
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