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Tag Archives: Tunnel

777X’s Trans-Sonic & Sub-Sonic Wind Tunnel Testing Underway

16 Thursday Jan 2014

Posted by theflyingengineer in Manufacturer, Technical

≈ Leave a comment

Tags

777, Boeing, testing, Tunnel, Wind, X

Left: Subsonic wind tunnel testing at QinetiQ's facility in Farnborough, U.K, Right: Trans-sonic wind tunnel testing at Boeing's Transonic Wind Tunnel in Seattle

Left: Subsonic wind tunnel testing at QinetiQ’s facility in Farnborough, U.K, Right: Trans-sonic wind tunnel testing at Boeing’s Transonic Wind Tunnel in Seattle

Boeing announced that testing has begun at the Boeing Transonic Wind Tunnel in Seattle to further validate 777X high-speed performance projections. Data from the high-speed tests will help engineers with the configuration development of the airplane, validate computational fluid dynamics (CFD) predictions and support preliminary loads cycle development.

Subsonic wind tunnel testing on the 777X started on Dec. 5, 2013 at QinetiQ’s test facility in Farnborough, U.K., to test the airplane models’ performance at low speeds such as those experienced at takeoff and landing, and at different non-clean configurations, notably with the high lift devices such as flaps and slats.

“We are on track to complete our top-level design in 2014 and reach firm configuration in 2015,”, Terry Beezhold, vice president and chief project engineer of the 777X program, said, back in Dec 2013. “Wind tunnel testing will validate our performance models and generate a vast amount of data that our engineering teams will use to design the airplane in this phase of development.”

The Boeing 777X program, which includes the 777-8X and 777-9X aircraft, is yet to be formally christened.

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