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Aerodynamics & Hydrodynamics from MotherNature

 
 
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Old 03-09-2008, 11:50 AM   #1
brian eiland
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Aerodynamics & Hydrodynamics from MotherNature

,.....consider these unusual findings from Mother Nature:

DURHAM, N.C. -- Wind tunnel tests of scale-model humpback whale flippers have revealed that the scalloped, bumpy flipper is a more efficient wing design than is currently used by the aeronautics industry on airplanes. The tests show that bump-ridged flippers do not stall as quickly and produce more lift and less drag than comparably sized sleek flippers.

The tests were reported by biomechanicist Frank Fish of West Chester University, Pa., fluid dynamics engineer Laurens Howle of the Pratt School of Engineering at Duke University and David Miklosovic and Mark Murray at the U.S. Naval Academy. They reported their findings in the May 2004 issue of Physics of Fluids, published in advance online on March 15, 2004.

In their study, the team first created two approximately 22-inch-tall scale models of humpback pectoral flippers -- one with the characteristic bumps, called tubercles, and one without. The models were machined from thick, clear polycarbonate at Duke University. Testing was conducted in a low speed closed-circuit wind tunnel at the U.S. Naval Academy in Annapolis, Md.

The sleek flipper performance was similar to a typical airplane wing. But the tubercle flipper exhibited nearly 8 percent better lift properties, and withstood stall at a 40 percent steeper wind angle. The team was particularly surprised to discover that the flipper with tubercles produced as much as 32 percent lower drag than the sleek flipper.

“The simultaneous achievement of increased lift and reduced drag results in an increase in aerodynamic efficiency,” Howle explains.

This new understanding of humpback whale flipper aerodynamics has implications for airplane wing and underwater vehicle design. Increased lift (the upward force on an airplane wing) at higher wind angles affects how easily airplanes take off, and helps pilots slow down during landing.

Improved resistance to stall would add a new margin of safety to aircraft flight and also make planes more maneuverable. Drag -- the rearward force on an airplane wing -- affects how much fuel the airplane must consume during flight. Stall occurs when the air no longer flows smoothly over the top of the wing but separates from the top of the wing before reaching the trailing edge. When an airplane wing stalls, it dramatically loses lift while incurring an increase in drag.

As whales move through the water, the tubercles disrupt the line of pressure against the leading edge of the flippers. The row of tubercles sheer the flow of water and redirect it into the scalloped valley between each tubercle, causing swirling vortices that roll up and over the flipper to actually enhance lift properties.

“The swirling vortices inject momentum into the flow,” said Howle. “This injection of momentum keeps the flow attached to the upper surface of the wing and delays stall to higher wind angles.”

“This discovery has potential applications not only to airplane wings but also on the tips of helicopter rotors, airplane propellers and ship rudders,” said Howle.

The purpose of the tubercles on the leading edge of humpback whale flippers has been the source of speculation for some time, said Fish. “The idea they improved flipper aerodynamics was so counter to our current doctrine of fluid dynamics, no one had ever analyzed them,” he said.

http://www.pratt.duke.edu/news/?id=101
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Old 03-09-2008, 01:16 PM   #2
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There's a paragraph at Harvard professor Michael Brenner's pages at
http://www.seas.harvard.edu/brenner/Research%203.html

"We have been interested in understanding the aerodynamic mechanism for this stall-delay. Recent work with Ernst van Nierop and Silas Alben demonstrates the mechanism for the observed increase in stall angle. Although the bumps have been compared to vortex generators, we propose a different mechanism: we demonstrate that the bumps alter the pressure distribution on the wing such that separation of the boundary is delayed behind bumps; this ultimately leads to a gradualonset of stall and higher stall angle. Our mechanism predicts that as the amplitude of the bumps is increased, the lift curve flattens out leading to potentially desirable control properties. Model airplane builders have started experimenting with this type of wing shape."
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Old 03-09-2008, 03:14 PM   #3
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Hopefully this goes somewhere. When vortex generators were introduced as STC'd kits on some aircraft, a lot of off the record experimentation was done.
Much of it was.."well, if a row works well here then what'll happen if I put a couple further back" type stuff. They got stuck here there and everywhere.
Yes Virginia, there is a Santa Claus, and Yes there are still out of the way places on this planet where the curious try out all kinds of things without the proper approvals and inspections just to satisfy their curiosity. Even tried out on prop blade tips to see if they'd change the loud bark that is produced when the tip goes supersonic. The experimentation stopped or went completely off radar quite suddenly and I haven't heard a peep in a long time.
Hmmm. Lumps and bumps on a laminar flow wing.... Could be interesting.
Nature does have a way of being subtle and only letting the observant hear her say: Been there, done that.
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