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Aerospace Structures and Elements - Projekt

ED110125Required Modules4 ECTSEnglishsummer semesterLehrstuhl für Strukturauslegung in der Luft- und Raumfahrt (Prof. Daoud)
AI-edited module sheet. Based on the TUMonline module description, edited for readability.Original in TUMonline

What it is about

You engage with the structural principles of aircraft and spacecraft: materials, lightweight design, stability, strength, and finite element modeling. In the end you will be able to appraise components and construction methods of wing and fuselage structures, explain loads and failure mechanisms, perform estimates of strength and stability, and undertake simple structural design.

What you will be able to do

  • Compare current technologies and structural concepts
  • Differentiate essential components and design principles
  • Perform strength and stability assessments
  • Explain failure mechanisms of structures
  • Calculate external and internal aircraft loads and use them for component design
  • Differentiate and evaluate construction methods for wing and fuselage structures

What the module consists of

  • VorlesungDelivery of theoretical foundations and derivation of relevant concepts
  • ÜbungWorking through example problems, discussion of plausibility, and illustration with case studies
  • Projekt/AbgabenIndividual project with structural analyses, redesigns and simulations

Teaching method

  • Vortrag/PräsentationIntroduction and derivation of theoretical foundations; slides provided in advance
  • Eigenstudium mit empfohlener LiteraturDeepening of terminology and relationships, preparation for exercises and project
  • Übungsrechnungen am Tablet-PCStep-by-step solution of tasks for discussion and plausibility check
  • Fallbeispiele und AnschauungsobjekteIllustration of practice-relevant aspects
  • Freiwillige Hausübungen mit LösungenAdditional practice opportunities to consolidate the material
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Official page in TUMonline · Details are not binding.