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|a Multidisciplinary design analysis and optimization of aerospace composite materials /
|c [edited by] Charles Lu.
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|a Warrendale, Pennsylvania, USA :
|b SAE International,
|c [2020]
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|a Overall design methodology. Chapter 1. Investigation of multi-disciplinary optimisation for aircraft preliminary design -- Weight analysis. Chapter 2. Refined preliminary weight estimation tool for airplane wing and tail -- Structural analysis. Chapter 3. Static/fatigue structural behaviour of damaged stiffened composite plates for UAS applications -- Aerodynamic analysis. Chapter 4. Development of variable camber continuous trailing edge flap for performance adaptive aeroelastic wing -- Thermal analysis. Chapter 5. Heat pipe embedded carbon fiber reinforced polymer composite enclosures for avionics thermal management -- Acoustic analysis. Chapter 6. Uncertainty modeling for aircraft interior noise -- composites transmission loss optimization -- Lightening analysis. Chapter 7. More about lightning induced effects on systems in a composite aircraft -- Fire analysis. Chapter 8. Fire resistant composites -- Reliability analysis. Chapter 9. Reliability analysis of composite inflatable space structures considering fracture failure -- Sustainability analysis. Chapter 10. A conceptual framework for value chain analysis of end of life aircraft treatment in the context of sustainable development.
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|a A collection of ten SAE technical papers focusing on the design analysis of aerospace composite structures from the perspective of various disciplines.
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|a Includes bibliographical references.
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|a Knovel
|b ACADEMIC - Aerospace & Radar Technology
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|a Aerospace engineering.
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|a Composite materials.
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|a Aérospatiale (Ingénierie)
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|a Composites.
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|a composite material.
|2 aat
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|a Aerospace engineering.
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|a Composite materials.
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|a Lu, Y. Charles,
|e editor.
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|c Original
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