1970
DOI: 10.2514/3.44193
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Jet circulation control airfoil for VTOL rotors

Abstract: Based on the potential flow theory calculation, the capacity of the air supply, the limitation of the internal pressure of the model and the limitation due to the compressibility effect of the jet stream at high velocities, the elliptical airfoils of 18 and 12% thickness ratios were designed and constructed. Experimental investigations for both models with trailing-edge jets include force and pitching moment measurements. In addition, static pressure measurements were made in both span wise and chord wise dire… Show more

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