Expressions derived for representative group of wing plan forms; analysis based on edge suction theory as well as linearized potential theory and applied to triangular, trapezoidal, rectangular, and sweptback plan forms without dihedral.
Yawing moment due to sideslip of triangular, trapezoidal, and related plan forms in supersonic flow
Nat Advisory Committee Aeronautics -- Tech Note
1949
65 pages
Diagrs, Charts
Report
English
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Rolling moment due to sideslip of triangular, trapezoidal, and related plan forms in supersonic flow
Engineering Index Backfile | 1948
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