תקציר
The rapid convergence characteristics and high accuracy of the three-dimensional piecewise continuous kernel function method are tested on a nonplanar configuration. The nature of the singularity of the three-dimensional kernel function for the nonplanar configuration is examined and anomalies associated with almost adjoining lifting surfaces are explained. Applications are made using the standard AGARD wing-tail configuration and the interference aerodynamic forces are compared with results obtained using other numerical methods.
שפה מקורית | אנגלית |
---|---|
עמודים (מ-עד) | 1043-1048 |
מספר עמודים | 6 |
כתב עת | Journal of Aircraft |
כרך | 22 |
מספר גיליון | 12 |
מזהי עצם דיגיטלי (DOIs) | |
סטטוס פרסום | פורסם - דצמ׳ 1985 |
פורסם באופן חיצוני | כן |