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The innovative Boeing (NYSE: BA) Blended Wing Body (BWB) research aircraft -- designated the X-48B -- flew for the first time last week at NASA's Dryden Flight Research Center at Edwards Air Force Base in California.
The 21-foot wingspan, 500-pound unmanned test vehicle took off for the first time at 8:42 a.m. Pacific Daylight Time on July 20 and climbed to an altitude of 7,500 feet before landing 31 minutes later.
"We've successfully passed another milestone in our work to explore and validate the structural, aerodynamic and operational efficiencies of the BWB concept," said Bob Liebeck, BWB program manager for Boeing Phantom Works, the company's advanced R&D unit. "We already have begun to compare actual flight- test data with the data generated earlier by our computer models and in the wind tunnel."
The X-48B flight test vehicle was developed by Boeing Phantom Works in cooperation with NASA and the U.S. Air Force Research Laboratory to gather detailed information about the stability and flight-control characteristics of the BWB design, especially during takeoffs and landings. Up to 25 flights are planned to gather data in these low-speed flight regimes. Following completion of low-speed flight testing, the X-48B likely will be used to test the BWB's low-noise characteristics, as well as BWB handling characteristics at transonic speeds.
Two X-48B research vehicles have been built. The vehicle that flew on July 20 is Ship 2, which also was used for ground and taxi testing. Ship 1, a duplicate of Ship 2, completed extensive wind tunnel testing in 2006 at the Old Dominion University NASA Langley Full-Scale Tunnel in Virginia. Ship 1 will be available for use as a backup during the flight test program.
Three turbojet engines enable the composite-skinned research vehicle to fly up to 10,000 feet and 120 knots in its low-speed configuration. Modifications would need to be made to the vehicle to enable it to fly at higher speeds. The unmanned aircraft is remotely piloted from a ground control station in which the pilot uses conventional aircraft controls and instrumentation while looking at a monitor fed by a forward-looking camera on the aircraft.
The Boeing BWB design resembles a flying wing, but differs in that the wing blends smoothly into a wide, flat, tailless fuselage. This fuselage blending helps to get additional lift with less drag compared to a circular fuselage. This translates to reduced fuel use at cruise conditions. And because the engines mount high on the back of the aircraft, there is less noise inside and on the ground when it is in flight.
For more information: http://www.boeing.com/

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