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Vibration response of geometrically nonlinear elastic beams to pulse and impact loading
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Liebowitz, H. |
| Copyright Year | 1983 |
| Description | The governing equations for the geometrically nonlinear deformation of elastic beams subjected to dynamic bending loads are developed and solved for various initial conditions. Of primary interest is the response to pulse loading and simulated impact. Both transient and several cycle solutions are generated for the free vibration response to pulse loading. The results obtained are compared to a first mode analysis approximation. A model is developed to simulate impact loading by the distribution of additional mass to the elastic system and subjecting it to a velocity pulse. The governing equations are solved using second order finite differences in space and time. The solutions obtained are in reasonable agreement with experimental results. |
| File Size | 4293621 |
| Page Count | 34 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19840004459 |
| Archival Resource Key | ark:/13960/t3rv5d03c |
| Language | English |
| Publisher Date | 1983-10-07 |
| Access Restriction | Open |
| Subject Keyword | Structural Mechanics Deformation Flat Plates Beams Supports Bending Laminates Impact Loads Aircraft Structures Impact Damage Foreign Bodies Elastic Bodies Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |