Loading...
Please wait, while we are loading the content...
Similar Documents
Advanced turboprop vibratory characteristics
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Fulton, G. B. Srinivasan, A. V. |
| Copyright Year | 1984 |
| Description | The assembly of SR5 advanced turboprop blades to develop a structural dynamic data base for swept props is reported. Steady state blade deformation under centrifugal loading and vibratory characteristics of the rotor assembly were measured. Vibration was induced through a system of piezoelectric crystals attached to the blades. Data reduction procedures are used to provide deformation, mode shape, and frequencies of the assembly at predetermined speeds. |
| File Size | 14578932 |
| Page Count | 107 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19860015222 |
| Archival Resource Key | ark:/13960/t9p31qn9f |
| Language | English |
| Publisher Date | 1984-04-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Propulsion And Power Propeller Blades Dynamic Structural Analysis Performance Tests Propeller Fans Prop-fan Technology Vibrational Stress Vibration Tests Data Reduction Data Bases 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 |