| dc.contributor.author | Stettner, Martin | en_US |
| dc.contributor.author | Schrage, Daniel P. | en_US |
| dc.contributor.author | Peters, D. A. (David A.) | en_US |
| dc.date.accessioned | 2005-05-26T14:05:17Z | |
| dc.date.available | 2005-05-26T14:05:17Z | |
| dc.date.issued | 1994-02 | en_US |
| dc.identifier.uri | http://hdl.handle.net/1853/6413 | |
| dc.description | Presented at the American Helicopter Society Aeromechanics Specialists Meeting, San Francisco, CA, January 19-21, 1994. | en_US |
| dc.description.abstract | The Peters/He Finite State Wake Model is described in its application to fixed wing aerolasticity. Expressions for coupling this model with a wing, aerodynamically represented by a flat plate with a trailing edge flap, are developed, and fidelity issues are discussed. An application is presented where the wing/wake system is coupled to a proprotor model. The effects of unsteady wing aerodynamics on damping of this system are investigated. It is found that wake effects are small as a result of generally low damping levels in the system due to wing aerodynamic damping. | en_US |
| dc.format.extent | 156963 bytes | |
| dc.format.mimetype | application/pdf | |
| dc.language.iso | en_US | en_US |
| dc.publisher | Georgia Institute of Technology | en_US |
| dc.relation.ispartofseries | ASDL;AHS-0194-66 | en_US |
| dc.subject | Tilt rotor aircraft | en_US |
| dc.subject | Aerodynamics | en_US |
| dc.subject | Rotary wings | en_US |
| dc.subject | Aeroelasticity | en_US |
| dc.subject | Control surfaces | en_US |
| dc.subject | Unsteady aerodynamics | en_US |
| dc.subject | Wakes | en_US |
| dc.subject | Damping | en_US |
| dc.title | Application of a State-Space Wake Model to Tiltrotor Wing Unsteady Aerodynamics | en_US |
| dc.type | Paper | |
