Kontakt
Wie einkaufen
Versand
Kaufberater
Fatigue Response of Thin Stiffened Aluminum Cracked Panels Repaired with Bonded Composite Patches
Englisch
129 b
Bis zu 30 Tage Rückgaberecht
Kunden kauften auch
/
Broschur
25.59
€
/
Broschur
54.99
€
This research investigated the fatigue response of precracked and patched 2024- T3 Aluminum panels with stiffeners. The patches were single-sided, partially bonded, unidirectional three ply boron/epoxy. Stiffeners were 2024-T3 aluminum and were riveted as well as bonded on. Stiffeners were oriented in the direction of loading and were separated by a certain distance, with the crack centered between two stiffeners. Two stiffener separation distances, or spacings, were used--one to simulate transport aircraft fuselage stiffeners and one to simulate transport aircraft wing stiffeners. Disbonds were introduced into the adhesive bondline by inserting teflon strips. Three disbond configurations were investigated--a crack tip disbond (CTD) located at the edge of the patch in the path of crack propagation, a full-width disbond (FWD) covering the entire crack, and an end disbond (ED) located at each end of the patch and covering the full width. Each repaired panel was subjected to tension/tension cyclic fatigue with an R ratio of 0.05 and a maximum stress of 120 MPa.
Informationen zum Buch
Englisch
Kategorie
Verschenken Sie dieses Buch noch heute
Es ist ganz einfach
1 Legen Sie das Buch in Ihren Warenkorb und wählen Sie den Versand als Geschenk 2 Wir schicken Ihnen umgehend einen Gutschein 3 Das Buch wird an die Adresse des beschenkten Empfängers geliefertDas könnte Sie auch interessieren
/
Hardcover
197.79
€
/
Broschur
17.89
€
/
Hardcover
101.79
€
/
Hardcover
34.99
€
/
Hardcover
19.99
€
Hallo! Ich bin Libroamiko, dein Buchberater.
Wie kann ich dir helfen?