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Ground shake test of the boeing model 360 helicopter airframe
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Gabel, R. Reed, D. A. |
| Copyright Year | 1989 |
| Description | Boeing Helicopters, together with other U.S. Helicopter manufacturers, is engaged in a finite element applications program designed to emplace in the U.S. a superior capability to utilize finite element analysis models in support of helicopter airframe structurel design. This program was given the acronym DAMVIBS (Design Analysis Methods for VIBrationS). The test plan is reviewed and results are presented for a shake test of the Boeing Model 360 helicopter. Results of the test will serve as the basis for validation of a finite element vibration model of the helicopter. |
| File Size | 9611716 |
| Page Count | 350 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19890014549 |
| Archival Resource Key | ark:/13960/t9w13zt9h |
| Language | English |
| Publisher Date | 1989-03-01 |
| Access Restriction | Open |
| Subject Keyword | Structural Mechanics Finite Element Method Ground Tests Airframes Helicopters Boeing Aircraft Applications Programs Computers Mathematical Models Design Analysis Vibration Tests Abbreviations Computer Aided Design Structural Analysis Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
