Aerodynamic Multiobjective Design Exploration of a Flapping Airfoil Using a Navier-Stokes Solver
Author:
Affiliation:
1. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, Sagamihara, Kanagawa, 229-8510, Japan
2. University of Tokyo, Sagamihara, Kanagawa, 229-8510, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Electrical and Electronic Engineering,Computer Science Applications,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.35992
Reference25 articles.
1. Garrick, I. E. "Propulsion of a Flapping and Oscillating Airfoil," NACA Report 567, 1936.
2. Thrust generation due to airfoil flapping
3. Effects of Dynamic Stall on Propulsive Efficiency and Thrust of Flapping Airfoil
4. Optimization of Flapping Airfoils For Maximum Thrust and Propulsive Efficiency
5. Oscillating foils of high propulsive efficiency
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