The finite element method is used to calculate the spanwise variation of potential form drag of a wing at subsonic and supersonic speeds using linearly varying panels. The wing may be of arbitrary planform and nonplanar provided the wing panels are parallel to the aircraft axis.
Spanwise variation of potential form drag
1977-05-18
Report
No indication
English
Spanwise Variation of Potential Form Drag
NTIS | 1977
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