'Double-Bubble' Airliners Designed by MIT for NASA Could Trim Fuel Consumption by 70 Percent (http://www.popsci.com/technology/article/2010-05/mit-designed-double-bubble-airliners-could-trim-fuel-consumption-70-percent)

By Clay Dillow (http://www.popsci.com/category/popsci-authors/clay-dillow) Posted 05.17.2010 at 11:40 am[/URL]

http://www.popsci.com/files/imagecache/article_image_large/articles/MITplanes.jpg
MIT's D Series Concept (left) and H Series MIT/Aurora Flight Sciences



Automobile design has changed drastically over the last half century, and computers have gone from filling entire rooms to fitting neatly in our briefcases. The Boeing 737, however, has changed very little. An MIT team aims to bring aviation into the 21st century with two bold new designs for commercial airliners that could trim fuel use by up to 70 percent while increasing passenger capacity.

The designs -- dubbed D series and H series -- are part of a $2.1 million research contract from NASA to develop the next generation of subsonic airplanes (separate grants were given to Boeing and Lockheed Martin to design supersonic concepts). Competing with designs from GE Aviation, Boeing and Northrop Grumman, the object was to create a passenger jet that burns 70 percent less fuel, cuts emissions of nitrogen oxides by 75 percent, takes off from shorter runways, and reduces sound pollution.

MIT's solution: A "double bubble" architecture that relies on a dual fuselage design -- that is, two cylindrical structures placed side by side to make up the fuselage rather than a single tube-and-wing structure (such that a cross section would resemble two soap bubbles fused together). The design allows for a wider, shorter fuselage that should help passenger loading and unloading as well as increase seating capacity.

But the real innovation is in the engine placement. Rather than wing-mounted turbines that scoop up the untouched fast-moving air away from the fuselage, the tail-mounted D series engines suck up the slower-moving air coming off the wake of the fuselage. This Boundary Layer Ingestion (BLI) technique allows less fuel to be burned while generating the same amount of thrust, allowing the D series design to hit the 70 percent fuel reduction goals outlined by NASA.

NASA envisions aggressive designs like the D series taking flight by 2035, when air traffic is expected to double from current levels. To bridge the gap, MIT also mocked up an H series plane based on the same design principles but using current jet technology and conventional aluminums that achieves a 50 percent fuel burn and could serve as an alternative until something like the D series becomes standard.

There are drawbacks to both designs of course. The rear engine layout would increase engine stress, and both planes would travel about 10 percent slower than a 737. But given the fuel savings and reduced runway real estate needed to launch and land the D series, a small concession in flight time sounds pretty reasonable.

[[URL="http://web.mit.edu/newsoffice/2010/nplus3-0517.html"]MIT News (http://www.popsci.com/technology/article/2010-05/mit-designed-double-bubble-airliners-could-trim-fuel-consumption-70-percent?page=#comments)]

Very interesting article Commander. Love the H design. :)

The only two potential problems I can see with the design, and it would be interesting to see what Mr. A thinks about this, is the increased stress on the wings during take-off and landing because the engine weight does not counter balance the lift from the wings. The back-mounted engines were never favored for passenger airliners - if I'm not mistaken they were used in 727's, MD80's and a few Bombardier CRJ series. In case of the CRJ's, they have a very short wing span, which makes the bending moments more mangeable. Having said that, it looks like they've at least resolved the CG problem by putting a lot of the weight in the front to counter the engine weight at the back.

The 2nd and more serious problem is also during take-off, climb and landing where you have relatively high angles of attack and can potentially starve the engines for oxygen by putting them in the wake of the fuselage. Of course, these three instances are where you need your lift the most and any failure could be catastrophic. I really don't know how they're going to get around that unless they put place intakes on the side of the aircraft to redirect the air from the side of the fuselage to the top. That would be a major drag on the fuel saving design though - no pun intended on the drag! ;)

I get what you say, the answers should come from Rasoul, I personally thought that this wing design, especially the second one, wasnt suitable for commercial planes. They mention 2 drawbacks themselves with increased engine stress and being not as fast.

Actually I think with your second question, I think the point of the whole first design is having a very wide fuselage and providing extra lift, not having not enough of it.

The link to MIT is a bit longer article but not that detailed either.