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Finite element modeling of the higher harmonic controlled oh-6a helicopter airframe
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Ferg Sr., Douglas Toossi, Mostafa |
| Copyright Year | 1990 |
| Description | An MSC/NASTRAN finite element model of the higher harmonic control configured OH-6A helicopter fuselage was developed. This finite element model was verified by performing various model checkouts and correlation with results from a ground vibration test. |
| File Size | 1079353 |
| Page Count | 78 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19910008115 |
| Archival Resource Key | ark:/13960/t0dv6fj8t |
| Language | English |
| Publisher Date | 1990-10-01 |
| Access Restriction | Open |
| Subject Keyword | Structural Mechanics Finite Element Method Ground Tests Airframes Fuselages Mathematical Models Nastran Harmonic Control Vibration Tests Oh-6 Helicopter Structural Analysis 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 |