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Nonlinear analysis of damaged stiffened fuselage shells subjected to combined loads
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Bains, Jane C. Shore, Charles P. Rankin, Charles C. Starnes Jr., James H. Britt, Vicki O. Young, Richard D. |
| Copyright Year | 1994 |
| Description | The results of an analytical study of the nonlinear response of stiffened fuselage shells with long cracks are presented. The shells are modeled with a hierarchical modeling strategy that accounts for global and local response phenomena accurately. Results are presented for internal pressure and mechanical bending loads. The effects of crack location and orientation on shell response are described. The effects of mechanical fasteners on the response of a lap joint and the effects of elastic and elastic-plastic material properties on the buckling response of tension-loaded flat panels with cracks are also addressed. |
| File Size | 3585570 |
| Page Count | 31 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19950013083 |
| Archival Resource Key | ark:/13960/t3kx0b73x |
| Language | English |
| Publisher Date | 1994-09-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Design, Testing And Performance Cracks Bending Nonlinearity Fuselages Elastic Properties Lap Joints Buckling Loads Forces Internal Pressure Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
