Abstract
Through factual observations of the F-16, it has been found that a nonlinear structural damping (NSD) model based on dry friction would more likely be an individual or collective cause of limit cycle oscillations (LCO) over much wider Mach ranges than transonic LCO. Additional data suggest that priority should be given to NSD research. Towards this end, the development of a LCO prediction methodology using simpler aerodynamics with NSD and the pursuance of the understanding of LCO using high level CFD with NSD are proposed.
| Original language | English (US) |
|---|---|
| Title of host publication | Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference |
| Publisher | AIAA |
| Pages | 2148-2161 |
| Number of pages | 14 |
| Volume | 3 |
| State | Published - 1999 |
| Event | Proceedings of the 1999 AIAA/ASME/ASCE/AHS/ASC Structrures, Structural Dynamics, and Materials Conference and Exhibit - St. Louis, MO, USA Duration: Apr 12 1999 → Apr 15 1999 |
Other
| Other | Proceedings of the 1999 AIAA/ASME/ASCE/AHS/ASC Structrures, Structural Dynamics, and Materials Conference and Exhibit |
|---|---|
| City | St. Louis, MO, USA |
| Period | 4/12/99 → 4/15/99 |
ASJC Scopus subject areas
- Architecture