NASA, Boeing finish tests of 757 vertical tail with advanced technology

Nov 15, 2013
A full-sized tail from a 757 commercial aircraft was modified and equipped with tiny jets called "sweeping jet actuators" that blow air across the rudder surfaces. Credit: NASA Ames Research Center

NASA's Ames Research Center and NASA's Langley Research Center, in partnership with The Boeing Co., have completed wind tunnel testing of a full-scale Boeing 757 vertical tail model equipped with active flow control technology.

A major objective of the tests was to show active can enhance the performance of a enough to enable future designers to reduce the size of the structure for a whole family of airplanes. That could reduce the penalties related to the vertical tail that aircraft currently pay in drag and weight.

The testing, which began in early September and concluded Nov. 4, took place at the U.S. Air Force's Arnold Engineering Development Center's 40- by 80-foot wind tunnel at Ames in Moffett Field, Calif.

"This test campaign is a key component of NASA's Environmentally Responsible Aviation Project," said project manager Fay Collier. "The maturation of technologies such as active flow control, which will benefit aviation by improving fuel efficiency, reducing emissions and noise levels, is what NASA's aeronautics research is all about. The promising results of these wind tunnel tests and the following flight demonstration in 2015 undoubtedly will have an impact on future "green" aircraft designs," said Collier.

The flow control on the 757 vertical tail model comes from sweeping jet actuators, which are devices that essentially blow air in a sweeping motion along the span of the tail. NASA provided the actuators as part of a collaborative agreement under its Environmentally Responsible Aviation Project.

"NASA is proud to be a part of the research to advance this technology," said Thomas Edwards, director of aeronautics at Ames. "The tests were successful and the technology is now ready to move forward to benefit the traveling public."

The test vertical tail is an actual 757 vertical tail that came out of an aircraft bone yard in Arizona. With the help of the Boeing test and evaluation team, Advanced Technologies Inc. of Newport News, Va., modified and refurbished the tail into a wind tunnel model.

The wind tunnel tests enabled the Boeing and NASA team to observe "a wide array of flow control configurations across the whole low-speed flight envelope of the vertical tail," said Ed Whalen, Boeing Research & Technology program manager for the testing. The team will pick the most efficient and effective flow control configuration for future flight testing "to see how it performs in the real flight environment," Whalen said.

The flight testing will be aboard the Boeing ecoDemonstrator program 757 flight test aircraft. Boeing's ecoDemonstrator program will focus on improving environmental performance by bringing new technologies, materials and methods to implementation faster than ever before.

The combined and flight tests will represent the first full-scale demonstration of this active flow control technology, Whalen said. "That will give us insight into how the system works, how effective and efficient it is, things that we're not completely sure of at this point."

Active flow control involves the manipulation of a flow field – through the addition of energy—to improve the aerodynamic performance of an aircraft structure. Active flow control can enable the design of simpler, smaller and more aerodynamically efficient structures that help reduce aircraft weight, drag, and fuel consumption.

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User comments : 3

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rwinners
not rated yet Nov 16, 2013
Benefits??? In realistic percentages, please?
Macrocompassion
not rated yet Nov 16, 2013
Did this program include boundary-layer suction? Research into this kind of blc has shown drag reductions from the avoidance of turbulence (stabilization of the laminar boundry layer) of up to 60%.
antialias_physorg
5 / 5 (1) Nov 16, 2013
Benefits?

I'd also ask whether the plane stays steerable if the system fails (due to icing up. rain, electrical/mechanical failure of actuator surface) or what happens if it gets 'stuck' in an unfavorable position? Will the plane still be able to land safely? Or are we talking automatic crash scenario as in the case of reverse thrust?

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