Reduced frequency effects on the near-wake of an oscillating elliptic airfoil
Author:
Publisher
Springer Science and Business Media LLC
Subject
Mechanical Engineering
Link
http://link.springer.com/content/pdf/10.1007/BF03016519.pdf
Reference18 articles.
1. Chang, J. W. and Park, S. O., 2000.“Measurements in the Tip Vortex Roll-up Region of an Oscillating Wing,”AIAA Journal, Vol. 38, No. 6, pp. 1092–1095.
2. Chang, J. W., Yoon, Y. H. and Eun, H. B., 2003, “Near-Wake Characteristics of an Oscillating NACA 4412 Airfoil,”AIAA paper 2003–4086, 21st Applied Aerodynamics Conference. Orlando, Florida.
3. Chang, J. W. and Yoon, Y. H., 2002, “Camber Effects on the Near-Wake of Oscillating Airfoils, ”Journal of Aircraft, Vol. 39. No. 4. pp. 713–716.
4. Chang, J. W. and Park, S. O., 1999. “A Visualization Study of Tip Vortex Roll-up of an Oscillating Wing,”Journal of Flow Visualization and Image Processing, Vol. 6, pp. 79–87.
5. De Ruyck, J. and Hirsch, C., 1983, “Instantaneous Turbulent Profiles in the Wake of an Oscillating Airfoil,”AIAA Journal, Vol. 21, No. 5, pp. 641–642.
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