A Virtual Testing Approach for Honeycomb Sandwich Panel Joints in Aircraft Interior
Springer Berlin (Verlag)
978-3-662-60278-2 (ISBN)
lt;b>Ralf Seemann studied mechanical Engineering at TU Hamburg (TUHH) and at National University of Singapore. From 2011-2016 he worked as research engineer at the Institut of Product Development and Mechanical Engneering Design at TUHH. Since 2017 he works as stress & weight engineer at Diehl Aviation.
Introduction.- State of the art.- Overall concept of mechanical characterization.- Mechanical characterization on constituent level.- Mechanical characterization on structural element level.- Mechanical characterization on sub-component level.- Virtual testing approach for sandwich panel joints.- Development of novel sandwich panel joints.- Summary and outlook.- Literature.- Appendix A - Constituent level.- Appendix B - Structural element level.- Appendix C - Sub-component level.
Erscheinungsdatum | 05.03.2022 |
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Reihe/Serie | Produktentwicklung und Konstruktionstechnik |
Zusatzinfo | XVII, 201 p. 143 illus., 95 illus. in color. |
Verlagsort | Berlin |
Sprache | englisch |
Maße | 168 x 240 mm |
Gewicht | 380 g |
Themenwelt | Technik ► Bauwesen |
Technik ► Maschinenbau | |
Schlagworte | Aerospace Technology and Astronautics • Finite Element Method • Nomex Honeycomb • sandwich structures • virtual testing |
ISBN-10 | 3-662-60278-4 / 3662602784 |
ISBN-13 | 978-3-662-60278-2 / 9783662602782 |
Zustand | Neuware |
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