Fracture mechanics analyses of the slip-side joggle regions of wing-leading-edge panels

Authors

  • I. S. Raju
  • N. F. Knight
  • K. Song
  • D. R. Phillips

DOI:

https://doi.org/10.3221/IGF-ESIS.15.05

Abstract

The Space Shuttle wing-leading edge consists of panels that are made of reinforced carbon-carbon. Coating spallation was observed near the slip-side region of the panels that experience extreme heating. To understand this phenomenon, a root-cause investigation was conducted. As part of that investigation, fracture mechanics analyses of the slip-side joggle regions of the hot panels were conducted. This paper presents an overview of the fracture mechanics analyses.

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Section

Miscellanea

How to Cite

Fracture mechanics analyses of the slip-side joggle regions of wing-leading-edge panels. (2013). Frattura Ed Integrità Strutturale, 5(15), pages 35-49. https://doi.org/10.3221/IGF-ESIS.15.05