| タイトル | An approach to constrained aerodynamic design with application to airfoils |
| 本文（外部サイト） | http://hdl.handle.net/2060/19930003133 |
| 著者（英） | Campbell, Richard L. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1992-11-01 |
| 言語 | eng |
| 内容記述 | An approach was developed for incorporating flow and geometric constraints into the Direct Iterative Surface Curvature (DISC) design method. In this approach, an initial target pressure distribution is developed using a set of control points. The chordwise locations and pressure levels of these points are initially estimated either from empirical relationships and observed characteristics of pressure distributions for a given class of airfoils or by fitting the points to an existing pressure distribution. These values are then automatically adjusted during the design process to satisfy the flow and geometric constraints. The flow constraints currently available are lift, wave drag, pitching moment, pressure gradient, and local pressure levels. The geometric constraint options include maximum thickness, local thickness, leading-edge radius, and a 'glove' constraint involving inner and outer bounding surfaces. This design method was also extended to include the successive constraint release (SCR) approach to constrained minimization. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 93N12321
NASA-TP-3260
L-17108
NAS 1.60:3260 |
| 権利 | No Copyright |
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