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Current progress of a finite element computational fluid dynamics prediction of flutter for the aerostructures test wing
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Arena Jr., Andrew S. |
| Copyright Year | 2002 |
| Description | This progress report focuses on the use of the STructural Analysis RoutineS suite program, SOLIDS, input for the AeroStructures Test Wing. The AeroStructures Test Wing project as a whole is described. The use of the SOLIDS code to find the mode shapes of a structure is discussed. The frequencies, and the structural dynamics to which they relate are examined. The results of the CFD predictions are compared to experimental data from a Ground Vibration Test. |
| File Size | 538999 |
| Page Count | 12 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20020044748 |
| Archival Resource Key | ark:/13960/t3jx3b202 |
| Language | English |
| Publisher Date | 2002-01-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Finite Element Method Wings Computational Fluid Dynamics Structural Vibration Boundary Conditions Flutter Analysis Vibration Tests Aircraft Structures Computer Programs Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
