Multifidelity Approaches for the Computational Analysis and Design of Effective Flapping Wing Vehicles
Author:
Affiliation:
1. Massachusetts Institute of Technology
2. Department of Ecology and Evolutionary Biology and Division of Engineering, Brown University
3. Division of Engineering, Brown University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2008-518
Reference54 articles.
1. 1Hall, K. C., and Hall, S. R., Minimum induced power requirements for flapping flight Journal of Fluid Mechanics, 1996, Vol.323, pp.285-315.
2. A Numerical Exploration of Parameter Dependence in Power Optimal Flapping Flight
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