Wings are treated on assumption that flow potentials in planes at right angles to long axis of airfoils are similar to corresponding 2-dimensional potentials; pressure distributions caused by downward acceleration, pitching, rolling, sideslipping, and yawing are obtained for wings with and without dihedral; stability derivatives calculated from these distributions are expected to apply at both subsonic and supersonic speeds.
Stability derivatives of low-aspect-ratio triangular wings at subsonic and supersonic speeds
Nat Advisory Committee Aeronautics -- Tech Note
1947
34 pages
Report
English
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Stability derivatives of triangular wings at supersonic speeds
Engineering Index Backfile | 1948
|Stability derivatives of triangular wings at supersonic speeds
Engineering Index Backfile | 1948
|