Practical Analysis of Aircraft Composites

Practical Analysis of Aircraft Composites

<i><b>Practical Analysis of Aircraft Composites</b></i> is a comprehensive guide to the analysis of composite aircraft materials,combining theory with proven practical approaches. Invaluable to both practicing professionals and academics, <b><i>Practical Analysis of Aircraft Composites</i></b> covers a wide variety of topics including:<ul><li>Basic mechanics of composite materials</li><li> Principles of Classical Laminate Theory</li><li>Unnotched strength prediction and notched strength prediction</li><li> Analysis methods for mechanically fastened joints</li><li> Bonded joint analysis for both metal and composite adherends</li><li> Stability solutions for laminated plates and built-up structures</li><li> Composite beams and sandwich structures</li><li> Unique mechanical properties of composites</li><li> Structural requirements and structural substantiation for aircraft composites</li><li> Practical aspects for Durability and Damage Tolerance (DaDT)</li><li> Standard design practices for laminates, joints, and sandwich structures</li></ul>