Uncovering the physics of flapping flat plates with artificial evolution

By Michele Milano, Morteza Gharib. Journal of Fluid Mechanics, 2005

133 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Computational Mechanics, Nature and Landscape Conservation

View Paper: https://www.semanticscholar.org/paper/36b9b8ae4b9e39f120d0f1743fed788c0c02936a

How researchers see this paper

The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.

In Aerospace Engineering

1. Chang-kwon Kang
2. Peter G. Madden
3. Hikaru Aono
4. Wei Shyy
5. George V. Lauder
6. Carlos E. S. Cesnik
7. Hao Liu
8. Pat Trizila

In Computational Mechanics

1. Wei Shyy
2. Kunihiko Taira
3. Chang-kwon Kang
4. Hikaru Aono
5. Tim Colonius
6. Carlos E. S. Cesnik
7. George V. Lauder
8. Hao Liu

In Nature and Landscape Conservation

1. Peter G. Madden
2. George V. Lauder
3. James L. Tangorra
4. Wei Shyy
5. Chang-kwon Kang
6. Hikaru Aono
7. Jeff D. Eldredge
8. Hao Liu

Citations in the corpus

• The Development of a Biologically Inspired Propulsor for Unmanned Underwater Vehicles (2007, background): “Once this design is made more robust, it will be an excellent candidate for an analysis that discovers, through artificial evolution [ 35 ] or other optimization methods, fin motions that are ideal for producing thrust and maneuvering forces.”
• Low-order phenomenological modeling of leading-edge vortex formation (2013, methodology): “Thus, it is not possible to use alternative shedding criteria, based on, for example, a formation number for the developing vortex [6,31].”
• The influence of airfoil kinematics on the formation of leading-edge vortices in bio-inspired flight (2009, background): “Milano and Gharib (2005) showed that maximum lift on a pitching and plunging plate was generated when ^”
• Three-dimensional flows around low-aspect-ratio flat-plate wings at low Reynolds numbers (2009, background): “Since the formation number is found to be a universal quantity for a variety of flows (e.g. Jeon & Gharib 2004; Milano & Gharib 2005), it is not surprising that t∗ is also fairly constant for the three-dimensional cases considered here.”
• Time-resolved reconstruction of the full velocity field around a dynamically-scaled flapping wing (2006, background): “This dimensionless distance is equivalent to the Formation number (Milano and Gharib 2005).”
• Recent progress in flapping wing aerodynamics and aeroelasticity (2010, background): “Milano and Gharib [66] measured the forces generated by pitching rectangular flat plate at approximately Re=4.”