A Virtual Testing Approach for Honeycomb Sandwich Panel Joints in Aircraft Interior

Ralf Seemann (Autor)

Buch | Hardcover

XVII, 201 Seiten

2019
Springer Berlin (Verlag)
978-3-662-60275-1 (ISBN)

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Virtual test methods can contribute to reducing the great effort for physical tests in the development of lightweight products. The present work describes an approach for virtual testing of sandwich panel joints based on the Building Block Approach and the Finite Elements Method. Building on a multitude of physical tests on sandwich materials and joints, adequate sub-models are developed, validated and synthesized to top-level models. The developed approach is eventually applied for the development of a novel sandwich panel joint.

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
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	553 g
Themenwelt	Technik ► Bauwesen
Themenwelt	Technik ► Maschinenbau
Schlagworte	Aerospace Technology and Astronautics • Finite Element Method • Nomex Honeycomb • sandwich structures • virtual testing
ISBN-10	3-662-60275-X / 366260275X
ISBN-13	978-3-662-60275-1 / 9783662602751
Zustand	Neuware