| タイトル | Reduction of computer usage costs in predicting unsteady aerodynamic loadings caused by control surface motions: Computer program description |
| 本文（外部サイト） | http://hdl.handle.net/2060/19820024441 |
| 著者（英） | Redman, M. C.; Petrarca, J. R.; Harrison, B. A.; Rowe, W. S. |
| 著者所属（英） | Boeing Commercial Airplane Co. |
| 発行日 | 1979-01-01 |
| 言語 | eng |
| 内容記述 | A digital computer program was developed to calculate unsteady loadings caused by motions of lifting surfaces with leading edge and trailing edge controls based on the subsonic kernel function approach. The pressure singularities at hinge line and side edges were extracted analytically as a preliminary step to solving the integral equation of collocation. The program calculates generalized aerodynamic forces for user supplied deflection modes. Optional intermediate output includes pressure at an array of points, and sectional generalized forces. From one to six controls on the half span can be accomodated. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 82N32317
NASA-CR-145354
NAS 1.26:145354 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/164954 |
