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Prediction of unsteady aerodynamic coefficients at high angles of attack
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Klein, Vladislav Murphy, Patrick C. Pamadi, Bandu N. Brandon, Jay M. |
| Copyright Year | 2001 |
| Description | The nonlinear indicial response method is used to model the unsteady aerodynamic coefficients in the low speed longitudinal oscillatory wind tunnel test data of the 0.1 scale model of the F-16XL aircraft. Exponential functions are used to approximate the deficiency function in the indicial response. Using one set of oscillatory wind tunnel data and parameter identification method, the unknown parameters in the exponential functions are estimated. The genetic algorithm is used as a least square minimizing algorithm. The assumed model structures and parameter estimates are validated by comparing the predictions with other sets of available oscillatory wind tunnel test data. |
| File Size | 846741 |
| Page Count | 14 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20010071442 |
| Archival Resource Key | ark:/13960/t5v74cs4n |
| Language | English |
| Publisher Date | 2001-01-11 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Algorithms Unsteady Aerodynamics Estimating Wind Tunnel Tests Exponential Functions Aerodynamic Coefficients F-16 Aircraft Low Speed Wind Tunnels Angle of Attack Parameter Identification Genetic Algorithms Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |