## Aeronautical Engineering for National Certificate, Volume 2 |

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### Contents

Fundamentals of Stress and Strain Complementary Shear | 25 |

Extensions to the Theory of Simple Bending Unsymmetrical | 40 |

Distribution of Shear Stress in Beams Solid Beams Certain | 50 |

Copyright | |

10 other sections not shown

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### Common terms and phrases

aeroplane aircraft structures applied load assumed axial bending moment diagram buckling calculate centroidal axis Chapter coefficient component compressive stress Concentrated Load considered constant cosec critical load cross-sectional area curved beam deflection determined diagonal direction distance elastic limit element end load end moments equal equilibrium Euler Example flange follows frame given gives Hence indicated in Fig inertia joints lateral load loment longitudinal M/EI magnitude maximum shear stress method modulus neutral axis normal obtained panel perpendicular pin-jointed plane polar diagram positive principal axes radian radius reactions shear centre shear flow shear force shown in Fig sign convention simple bending skin slope space frame stiffener strain energy strut supports tensile stress theorem thickness torque torsion tube Uniformly Distributed Load unit length vertical vertical deflection wing zero