| タイトル | Computation of wind tunnel wall effects for complex models using a low-order panel method |
| 本文（外部サイト） | http://hdl.handle.net/2060/19940025646 |
| 著者（英） | Ashby, Dale L.; Harris, Scott H. |
| 著者所属（英） | NASA Ames Research Center |
| 発行日 | 1994-02-01 |
| 言語 | eng |
| 内容記述 | A technique for determining wind tunnel wall effects for complex models using the low-order, three dimensional panel method PMARC (Panel Method Ames Research Center) has been developed. Initial validation of the technique was performed using lift-coefficient data in the linear lift range from tests of a large-scale STOVL fighter model in the National Full-Scale Aerodynamics Complex (NFAC) facility. The data from these tests served as an ideal database for validating the technique because the same model was tested in two wind tunnel test sections with widely different dimensions. The lift-coefficient data obtained for the same model configuration in the two test sections were different, indicating a significant influence of the presence of the tunnel walls and mounting hardware on the lift coefficient in at least one of the two test sections. The wind tunnel wall effects were computed using PMARC and then subtracted from the measured data to yield corrected lift-coefficient versus angle-of-attack curves. The corrected lift-coefficient curves from the two wind tunnel test sections matched very well. Detailed pressure distributions computed by PMARC on the wing lower surface helped identify the source of large strut interference effects in one of the wind tunnel test sections. Extension of the technique to analysis of wind tunnel wall effects on the lift coefficient in the nonlinear lift range and on drag coefficient will require the addition of boundary-layer and separated-flow models to PMARC. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 94N30151
NASA-TM-104019
A-93077
NAS 1.15:104019 |
| 権利 | No Copyright |
