Summary of the effect of multiple site damage on the linkup strength of 2024-T3 aluminum panels

Smith B. L., HIJAZİ A. L. A., Myose R. Y.

General Aviation Technology Conference and Exhibition, Wichita, KS, Amerika Birleşik Devletleri, 16 - 18 Nisan 2002, (Tam Metin Bildiri) identifier

  • Yayın Türü: Bildiri / Tam Metin Bildiri
  • Doi Numarası: 10.4271/2002-01-1534
  • Basıldığı Şehir: Wichita, KS
  • Basıldığı Ülke: Amerika Birleşik Devletleri
  • İstanbul Gelişim Üniversitesi Adresli: Evet

Özet

An bolted lap joints. Test results were obtained from 112 different panels. The modified linkup model is a significant improvement over the linkup model based on a comparison of predicted values with test values. Portions of this project have been previously published. However, the purpose of this paper is to present a summary of the results including details of the panel geometry, crack configurations, test results, and results from both the linkup model and the modified linkup model for the 112 panels. Copyright © 2002 Society of Automotive Engineers, Inc.