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User:SidewinderX/Sandbox/Boeing X-48

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X-48
X-48B
Role Experimental unmanned aerial vehicle
Manufacturer Boeing
First flight July 20, 2007 [1]
Primary user NASA

The X-48 is an experimental unmanned aerial vehicle built to investigate the characteristics of blended wing body (BWB) aircraft, a type of flying wing. It is currently under development by Boeing and NASA.

Development

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The Economist wrote the following in an article in June 2006:

"Boeing once toyed with a blended wing-body, a sort of flying wing, to produce dramatically better aerodynamics and fuel efficiency. Passengers would have sat in a wide cabin, rather like a small amphitheater. But tests with a mock-up produced such a negative reaction that the company dropped the technology, except for military refueling aircraft."[2]

In fact, the original concept of a blended wing-body goes back to the jet bombers the Germans were designing at the very end of World War II.[3] This concept was also developed at McDonnell Douglas in the 1990s, just prior to its merging into Boeing, and was presented during an annual Joint AIAA/ASME/SAE/ASEA Propulsion Conference in the US a few years ago. The McDonnell Douglas engineers were confident that their design had all the advantages mentioned, but their concept found no favor at Boeing. The most difficult problem they solved was that of ensuring passengers a safe and fast escape in case of an accident, since emergency door locations were completely different from those in a conventional aircraft.

Design

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In February 2007 Wired included the following in the article, Thinking Outside the Tube:

Ever since Boeing introduced the 707 in the 1950s, passenger jets have looked pretty much the same: long tubes with tails, engines mounted below the wings. That shape may one day be transformed into the graceful silhouette of a manta ray. In February, a 400-pound, 21-foot (6.4 m)-wide prototype of just such a bird will start practicing unmanned takeoffs, landings, and tricky slow-speed maneuvers at Edwards Air Force Base. Called the X-48B, it's a scaled-down model of a theoretical 500-ton, 240-foot (73 m)-wide blended-wing aircraft. Aeronautical engineers have long known that this design could be much quieter, more fuel efficient, and far roomier than a conventional cylinder. But recent advances—lightweight composite materials, fly-by-wire controls, sophisticated flight systems—have made building one of these planes more feasible. Commercial versions have been proposed—imagine a flying auditorium—but the X-48B is more likely to debut as a US military transport plane circa 2022."[4]

The BWB concept reportedly offers greater structural, aerodynamic and operating efficiencies than today's more conventional tube-and-wing designs. These features translate into greater range, fuel economy, reliability and life cycle savings, as well as lower manufacturing costs. They also allow for a wide variety of potential military and commercial applications.

 
Boeing X-48B flight test vehicle on display at the 2006 Edwards Airshow

The Boeing Phantom Works is developing the blended wing body aircraft concept in cooperation with the NASA Langley Research Center. In a continuing effort to study the flight characteristics of the BWB design, a small remote-controlled model has been successfully flown. The next step was to fly the X-48A in 2004, which was to be built at NASA Langley, but that program was later canceled.

Boeing Phantom Works is focusing current research on a pair of models, called the X-48B, which were built under contract by Cranfield Aerospace in the United Kingdom. Norman Princen, Boeing's chief engineer for the project, said, "Earlier wind-tunnel testing and the upcoming flight testing are focused on learning more about the BWB's low-speed flight-control characteristics, especially during takeoffs and landings. Knowing how accurately our models predict these characteristics is an important step in the further development of this concept."[5]

The X-48B has a 21-foot (6.4 m) wingspan, weighs 500-pound (230 kg), and is built from composite materials. They are powered by three small turbojet engines and are expected to fly at up to 120 kn (220 km/h) and reach an altitude of 10,000 feet (3,000 m).[5]

 
X-48B at first flight
 
X-48B at first flight, seen from below

NASA performed wind tunnel tests on Ship 1, an 8.5% scale model, at a facility shared by Langley and Old Dominion University in May 2006.[6] After the wind tunnel testing, the vehicle was shipped to NASA's Dryden Flight Research Center at Edwards Air Force Base where it will serve as a backup to Ship 2 for flight testing. Ground testing at Dryden began in November 2006, to validate the aircraft's systems integrity, telemetry and communications links, flight-control software and taxi and takeoff characteristics. Flight tests began on July 20, 2007 - the first flight reached an altitude of 7,500 feet MSL (2,286 m) and lasted 31 minutes.[7][8] The remotely-piloted aircraft was successfully stalled for the first time on 4 September, with fixed leading edge slats, a forward center of gravity, and 23-degree angle of attack (2° beyond the maximum coefficient of lift). Stall testing was repeated on 11 September with a NASA pilot at the console.[9]

Variants

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X-48A

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Canceled

X-48B

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two 8.5% scale aircraft, flew

X-48C

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New model modified with lessons learned from "b" model version, formed by modifying LSV1, one of the two X-48B platforms.

Those modifications include reducing the number of engines from three to two and the installation of noise-shielding vertical fins. The wind tunnel tests are assessing the aerodynamic effects of those modifications.

The aircraft, on its second visit, became the last thing to be tested in NASA LaRC's Full Scale Wind Tunnel

Source: http://www.nasa.gov/centers/langley/multimedia/iotw-x48c.html

Specifications (X-48B)

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Data from Risch, Tim, Cosentino, Gary, Regan, Christopher, Kisska, Michael, Princen, Norman (2009). X-48B Flight-Test Progress Overview. 47th AIAA Aerospace Sciences Meeting, 5 - 8 Jan 2009, Orlando, Florida. AIAA 2009-934.

General characteristics

  • Crew: Unmanned
  • Wingspan: 20 ft 5 in (6.22 m)
  • Gross weight: 525 lb (238 kg)
  • Powerplant: 3 × JetCat USA P200 (modified) , 54 lbf (0.24 kN) thrust each

Performance

  • Endurance: 0.5 hours


See also

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Aircraft of comparable role, configuration, and era

References

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  1. ^ Risch, Tim, Cosentino, Gary, Regan, Christopher, Kisska, Michael, Princen, Norman (2009). X-48B Flight-Test Progress Overview. 47th AIAA Aerospace Sciences Meeting, 5 - 8 Jan 2009, Orlando, Florida. AIAA 2009-934.
  2. ^ "Aircraft emissions" (fee required). The Economist. 2006-06-08. Retrieved 2007-04-11.
  3. ^ Herwig, Dieter (2000). Luftwaffe Secret Projects: Strategic Bombers 1935–1945. United Kingdom: Midland. ISBN 1857800923. {{cite book}}: Unknown parameter |coauthors= ignored (|author= suggested) (help)
  4. ^ Jacobs, Karrie (2007). "Thinking Outside the Tube". Wired. Retrieved 2007-04-11. {{cite news}}: Unknown parameter |month= ignored (help)
  5. ^ a b "Boeing to Begin Ground Testing of X-48B Blended Wing Body Concept". Mojave Desert News. 2006-10-27. Archived from the original on 2006-10-29. Retrieved 2007-04-11.
  6. ^ Barnstorff, Kathy (2006-05-04). "The X-48B Blended Wing Body". NASA Langley Research Center. Retrieved 2007-04-11.
  7. ^ "Boeing Flies Blended Wind Body Research Aircraft", Boeing, July 26, 2007.
  8. ^ "X-48B Blended Wing Body Research Aircraft Takes First Flight". NASA Press Release. 2007-07-26. Retrieved 2007-07-26.
  9. ^ Aviation Week & Space Technology, Vol. 169 No. 10, 15 Sept. 2008, "Stall Success", p. 20
Some of the above text came from:
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Category:Edwards Air Force Base Category:Jet aircraft Category:Multiple engine aircraft Category:United States experimental aircraft 2000-2009 Category:United States UAVs Category:Boeing aircraft

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