| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 775773 | International Journal of Fatigue | 2009 | 8 Pages |
Abstract
The composite bulkhead was designed and manufactured during the development of a new small Czech air carrier with pressurized fuselage. The bulkhead is honeycomb structure with carbon/epoxy skin. The technical and operational testing conditions, test facility possibilities and follow-up details related to the structure certification are stated. Results from residual strength test and results from advanced non-destructive testing are presented (Shearography method).
Related Topics
Physical Sciences and Engineering
Engineering
Mechanical Engineering
Authors
R. Růžek, J. BÄhal,