Tow-Steered Panels With Holes Subjected to Compression or Shear Loads

Tailoring composite laminates to vary the fiber orientations within a fiber layer of a laminate to address non-uniform stress states and provide structural advantages such as the alteration of principal load paths has potential application to future low-cost, light-weight structures for commercial t...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	Jegley, Dawn C., Tatting, Brian F., Guerdal, Zafer
Format:	Tagungsbericht
Sprache:	eng
Schlagworte:	Aircraft Design, Testing And Performance
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!