New Flow Control Techniques with Prepositioned Stationary or Vibrating Elliptical Wing at Low Speed and High Angle of Attack
Author:
Affiliation:
1. Associate Professor, School of Aeronautics, Northwestern Polytechnical Univ., Shaanxi, Xi’an 720072, PR China.
2. Ph.D. Student, School of Aeronautics, Northwestern Polytechnical Univ., Shaanxi, Xi’an 720072, PR China (corresponding author).
Publisher
American Society of Civil Engineers (ASCE)
Subject
Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering
Link
https://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0001433
Reference10 articles.
1. Abbott, I. H., and A. E. von Doenhoff. 1959. “Theory of wing sections.” In General information. New York: Dover.
2. Numerical simulation of vortex generators on a winglet control surface
3. Wake effect on a semi-active flapping foil based energy harvester by a rotating foil;Chen Y.;Comput. Fluids,2017
4. Numerical simulation of fluid flow and forced convection heat transfer from tandem circular cylinders using overset grid method
5. On the flow around two circular cylinders in tandem arrangement at high Reynolds numbers
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