Numerical Investigation of Wingtip Vortex Attenuation Using a Tip-Chipped Wing

Author:

ROH Nahyeon1,OH Sejong1,YEE Kwanjung2

Affiliation:

1. Department of Aerospace Engineering, Pusan National University

2. Department of Mechanical and Aerospace Engineering, Seoul National University

Publisher

Japan Society for Aeronautical and Space Sciences

Subject

Space and Planetary Science,Aerospace Engineering

Reference25 articles.

1. 1) Rossow, V. J.: Wake-vortex Separation Distances when Flight-path Corridors are Constrained, AIAA J., 33, 3 (1996), pp. 539–546.

2. 2) Rossow, V. J.: Lift-generated Vortex Wakes of Subsonic Transport Aircraft, Progress in Aerospace Sciences, Vol. 35, 1999, pp. 507–660.

3. 3) Tangler, J. L.: Schlieren and Noise Studies of Rotors in Forward Flight, 33rd American Helicopter Society Forum, Washington, DC, 1977.

4. 4) Yu, Y. H., Gmelin, B., Splettstoesser, W., Philippe, J. J., and Prieur, J.: Reduction of Helicopter Blade-Vortex Interaction Noise by Active Rotor Control Technology, Progress in Aerospace Sciences, Vol. 33, 1997, pp. 647–687.

5. 5) Rayleigh, L.: On the Dynamics of Revolving Fluids, Proc. R. Soc. London Ser. A, 93 (1917), pp. 148–154.

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