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Airframe structural dynamic considerations in rotor design optimization
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Kvaternik, Raymond G. Murthy, T. Sreekanta |
| Copyright Year | 1989 |
| Description | An an overview and discussion of those aspects of airframe structural dynamics that have a strong influence on rotor design optimization is provided. Primary emphasis is on vibration requirements. The vibration problem is described, the key vibratory forces are identified, the role of airframe response in rotor design is summarized, and the types of constraints which need to be imposed on rotor design due to airframe dynamics are discussed. Some considerations of ground and air resonance as they might affect rotor design are included. |
| File Size | 1218916 |
| Page Count | 28 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19900002741 |
| Archival Resource Key | ark:/13960/t42r8r026 |
| Language | English |
| Publisher Date | 1989-08-01 |
| Access Restriction | Open |
| Subject Keyword | Structural Mechanics Dynamic Structural Analysis Vibration Airframes Rotor Blades Turbomachinery Helicopters Optimization 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 |
