Northrop Grumman Selected To Design First-Ever 'Oblique Flying Wing' | Aero-News Network
Aero-News Network
RSS icon RSS feed
podcast icon MP3 podcast
Subscribe Aero-News e-mail Newsletter Subscribe

Airborne Unlimited -- Most Recent Daily Episodes

Episode Date

Airborne-Monday

Airborne-Tuesday

Airborne-Wednesday Airborne-Thursday

Airborne-Friday

Airborne On YouTube

Airborne-Unlimited-04.29.24

Airborne-Unlimited-04.23.24

Airborne-Unlimited-04.24.24 Airborne-FltTraining-04.25.24

Airborne-Unlimited-04.26.24

Sat, Mar 25, 2006

Northrop Grumman Selected To Design First-Ever 'Oblique Flying Wing'

Supersonic Aircraft Can Vary Wing Sweep For Most Efficient Performance

Northrop Grumman Corporation announced Friday the company has been selected by the US Department of Defense to design the first-ever supersonic flying wing aircraft that can vary the sweep of its wing for the most efficient flight performance.

The Defense Advanced Research Projects Agency (DARPA) has awarded a contract to Northrop Grumman's Integrated Systems sector for the first phase of its Oblique Flying Wing (OFW) program, which aims to design and conduct flight tests of an experimental tailless, supersonic, variable-sweep flying wing. DARPA's goal is to demonstrate that such aircraft are feasible so that similar designs can be considered for future military missions.

"The selection of Northrop Grumman for the Oblique Flying Wing program recognizes our long tradition of innovation and technical ability," said Charlie Guthrie, director of Advanced Capabilities Development for Integrated Systems' Western Region. "We look forward to working with DARPA and its government team to make aviation history."

The oblique flying wing would vary its wing sweep (the angle of the wing's leading edge relative to the direction of flight) depending on its speed. At low speeds (above) the wing sweep is relatively low, providing an efficient aerodynamic design.

At high speeds (below), right wing will sweep forward and the left wing will sweep back to reduce supersonic wave drag. The engines are mounted under the center of the wing.

The supersonic design envisioned by the OFW program offers potential benefits for missions requiring rapid deployment, long range and long endurance. In theory, an oblique flying wing could maximize its performance in every flight regime: takeoff or landing, high or low altitude, supersonic or subsonic speed.

During the program's first phase, which will conclude in November 2007, Northrop Grumman will conduct technology maturation to reduce the risk of the critical technologies associated with its OFW concepts and develop a preliminary design for the experimental aircraft. DARPA is providing funding of $10.3 million for this phase.

The preliminary design effort could be followed by a second phase to finalize the design, then build an experimental aircraft and flight test it. First flight of this "X-plane" is envisioned in 2010 or 2011.

With a "system-of-systems" approach, the Advanced Capabilities Development group at Northrop Grumman Integrated Systems brings world-class capabilities in system design, air-vehicle design, flight controls, vehicle management systems, network-enabling technologies and survivability. It also leverages other capabilities from across Northrop Grumman to offer innovative future solutions that meet emerging customer needs.

FMI: www.northropgrumman.com, www.darpa.mil

Advertisement

More News

Unfortunate... ANN/SportPlane Resource Guide Adds To Cautionary Advisories

The Industry Continues to be Rocked By Some Questionable Operations Recent investigations and a great deal of data has resulted in ANN’s SportPlane Resource Guide’s rep>[...]

ANN FAQ: Turn On Post Notifications

Make Sure You NEVER Miss A New Story From Aero-News Network Do you ever feel like you never see posts from a certain person or page on Facebook or Instagram? Here’s how you c>[...]

ANN's Daily Aero-Term (04.29.24): Visual Approach Slope Indicator (VASI)

Visual Approach Slope Indicator (VASI) An airport lighting facility providing vertical visual approach slope guidance to aircraft during approach to landing by radiating a directio>[...]

ANN's Daily Aero-Term (04.28.24): Airport Marking Aids

Airport Marking Aids Markings used on runway and taxiway surfaces to identify a specific runway, a runway threshold, a centerline, a hold line, etc. A runway should be marked in ac>[...]

ANN's Daily Aero-Linx (04.28.24)

Aero Linx: The Skyhawk Association The Skyhawk Association is a non-profit organization founded by former Skyhawk Pilots which is open to anyone with an affinity for the A-4 Skyhaw>[...]

blog comments powered by Disqus



Advertisement

Advertisement

Podcasts

Advertisement

© 2007 - 2024 Web Development & Design by Pauli Systems, LC