DEVELOPMENT AND TEST OF CERAMIC BONDED STAINLESS STEEL STRUCTURAL COMPONENTS
Abstract
Application of a ceramic-braze adhesive bonding process to a representative 17-7PH stainless steel aircraft component has been accomplished. Design allowables, weight analysis and a construction procedure pertinent to the application of a ceramic adhesive are also included. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 30, 1960
- Accession Number
- AD0257516
Entities
People
- Bruno Pascuzzi
- L.j. Workman
Organizations
- Boeing