Impact damage resistance and residual strength of laminated composite transport aircraft fuselage structure was studied experimentally. Techniques to quantify impact damage discretely and non-discretely are described. Experimental techniques to three-dimensionally map matrix damage and determine the sublaminate structure are illustrated. Impact damage was also quantified non-discretely, using characteristics of flexural wave propagation Strain distributions in compressively loaded impact damaged laminates were experimentally measured.
Experimental investigations into composite fuselage impact damage resistance and post-impact compression behavior
Experimentelle Untersuchungen bezüglich der Widerstandsfähigkeit gegen Stoßschäden von Flugzeugzellen aus Verbundwerkstoff und Kompressionsverhalten nach dem Stoß
1992
14 Seiten, 12 Bilder, 10 Quellen
Aufsatz (Konferenz)
Englisch
Impact Damage Resistance of Composite Fuselage Structure, Part 2
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