| タイトル | Design of transonic airfoils and wings using a hybrid design algorithm |
| 著者（英） | Campbell, Richard L.; Smith, Leigh A. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1987-10-01 |
| 言語 | eng |
| 内容記述 | A method has been developed for designing airfoils and wings at transonic speeds. It utilizes a hybrid design algorithm in an iterative predictor/corrector approach, alternating between analysis code and a design module. This method has been successfully applied to a variety of airfoil and wing design problems, including both transport and highly-swept fighter wing configurations. An efficient approach to viscous airfoild design and the effect of including static aeroelastic deflections in the wing design process are also illustrated. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 88A30767
SAE PAPER 871756 |
| 権利 | Copyright |
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