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Direct use of linear time-domain aerodynamics in aeroservoelastic analysis: aerodynamic model
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Gilbert, Michael G. Woods, J. A. |
| Copyright Year | 1990 |
| Description | The work presented here is the first part of a continuing effort to expand existing capabilities in aeroelasticity by developing the methodology which is necessary to utilize unsteady time-domain aerodynamics directly in aeroservoelastic design and analysis. The ultimate objective is to define a fully integrated state-space model of an aeroelastic vehicle's aerodynamics, structure and controls which may be used to efficiently determine the vehicle's aeroservoelastic stability. Here, the current status of developing a state-space model for linear or near-linear time-domain indicial aerodynamic forces is presented. |
| File Size | 393726 |
| Page Count | 14 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19910001003 |
| Archival Resource Key | ark:/13960/t3fz2605z |
| Language | English |
| Publisher Date | 1990-03-01 |
| Access Restriction | Open |
| Subject Keyword | Structural Mechanics Supersonic Flow Approximation Stability Subsonic Flow Unsteady Aerodynamics Eigenvalues Mathematical Models Time Aeroservoelasticity Aerodynamic Forces Aeroelasticity Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
