Centaur Nose Fairing Honeycomb Specimen Test,
Abstract
The purpose of the study was to determine Young's modulus of the facing material, and the core shear modulus in bending of the sandwich structure as a function of core orientation and loading systems. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Nov 13, 1961
- Accession Number
- AD0843804
Entities
People
- Vincent P. Panella
Organizations
- General Dynamics