ملخص
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.
اللغة الأصلية | الإنجليزيّة |
---|---|
الصفحات (من إلى) | 1043-1048 |
عدد الصفحات | 6 |
دورية | Journal of Aircraft |
مستوى الصوت | 22 |
رقم الإصدار | 12 |
المعرِّفات الرقمية للأشياء | |
حالة النشر | نُشِر - ديسمبر 1985 |
منشور خارجيًا | نعم |