Answers are grounded in this paper and cite their sources.
Summary Experiments performed on a low-speed circulation-controlled aerofoil are described. The aerofoil was of elliptic section with the circulation controlled by means of a jet blowing around the blunt trailing edge. Results for the lift, drag and pitching moment on the aerofoil are presented as functions of the blowing momentum coefficient and the angle of incidence. The results are for a two-dimensional aerofoil. Possible applications of this type of aerofoil are briefly discussed.
No takes yet. Share an insight, caveat, or question.
Kind et al. (1968) studied this question.
Synapse has enriched 10 related papers. Consider them for comparative context: