תקציר
The rapid convergence and high-accuracy characteristics of the three-dimensional piecewise continuous-kernel function method (PCKFM) are tested in the present work. The large number of numerical examples which are included herein is aimed at showing the computational efficiency of the method. Three-dimensional wings with no geometrical discontinuities along their spans (discontinuities are permitted at the wing root only) are treated. Problems associated with geometrical discontinuities (such as break points, control surfaces, etc.) are presented in Part HI of this work.
שפה מקורית | אנגלית |
---|---|
עמודים (מ-עד) | 352-355 |
מספר עמודים | 4 |
כתב עת | Journal of Aircraft |
כרך | 18 |
מספר גיליון | 5 |
מזהי עצם דיגיטלי (DOIs) | |
סטטוס פרסום | פורסם - מאי 1981 |
פורסם באופן חיצוני | כן |