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Tag Archives: Wing

Understanding the Ultimate Load-Wing test: A350

14 Tuesday Jan 2014

Posted by theflyingengineer in Flight Safety, General Aviation Interest, Manufacturer

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Tags

A350, flex, G, Load, test, Ultimate, Wing

A350_Ultimate_Load_Wing_Test

The Airbus A350 program achieved another milestone with the successful completion of the ultimate load wing test in December 2013. The ultimate load wing test is a test in which the wing is deflected to simulate the “ultimate” load, beyond or at which the wing is expected to fail.

The ultimate load is calculated as 2.5 times the maximum expected G load that the aircraft would ever encounter in its service life. For the Airbus A350, which is limited in the G loads that it may experience, by the Fly By Wire system to +2.5G, or with the FBW system deactivated, as is the case with a reversion to direct law, approximately between 3-3.5G with the aerodynamic limitations of the flight control surfaces. The ultimate load is then possibly between 7.5 – 8.75G.

Based on this G force, the expected wing flex due to aerodynamic loading is computed, and the wing of a static test airframe flexed (loaded) to the corresponding load. The wing is expected not to fail at this “ultimate” load equivalent flex. At this loading, the A350’s wings flexed in excess of 5 meters, while at a similarly scaled G loading, the A380’s wings flexed to close to 7.5 meters. The 787’s wing flexed up to 7.6 meters in a similar test, mandatory for certification.

In February 2006, the A380’s wing gave way just before the 1.5 times greater G load limit was reached.

Unlike in the past, aircraft manufacturers don’t seem to be stressing the wing beyond 1.5 times greater load, to the point of wing failure. The actual failure load may not be known.

According to Airbus, “This test was performed on the A350 XWB static test airframe that was built specifically to demonstrate the structural integrity of the airframe. The strains induced into the airframe were measured and monitored in real time using more than ten thousand measurement channels. The huge volume of data recorded was analysed and correlated to the structural computer models which have been used to design the airframe.”

With the comforting thought of a safe-enough wing, the first A350 airframe intended for commercial service, MSN6,  is being assembled for launch customer Qatar Airways.

Adding “Lift” to future Aero Engineers

07 Monday Oct 2013

Posted by theflyingengineer in General Aviation Interest

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Tags

Airbus, Education, Flap, University, Wing

Penn_StateAirbus donated an Airbus A300 “like-new flap” to Penn State’s College of Engineering a few days ago.Although an extremely small and seemingly insignificant part of a complex airliner, a flap is a great start to many research activities. Flaps, which are relied on during take-offs and landings, contribute to noise, drag, and performance penalties, and studies could possibly result in better flap configurations and/or design.

Barely a week back, The Federal Aviation Administration selected Penn State as part of a team of universities to form a new Air Transportation Center of Excellence for Alternative Jet Fuels and the Environment.

Airbus ended production of the twin-engine/twin-aisle A300 in 2007. According to Airbus, “The flap, which will be used for student research, has a catalog value of more than $900,000 dollars, and represents a major research opportunity for both undergraduate and graduate students in the College’s aviation and aerospace programs. Specifically, Penn State intends to use the flap in its aerospace structures courses. Study plans include installing strain gauges inside the flap to measure strain on the internal ribs and structure of the flap by applying loads to various locations of the flap.

Airbus defines flaps as, “Hinged structures on the trailing edge of fixed wing aircraft that are used to reduce speed and increase the angle of descent for landing, safely shortening takeoff and landing distances. Flaps do this by lowering stall speed and increasing drag.”

Students at the Pennsylvania State University Department of Aerospace Engineering will examine the design of the structure, and develop models to predict how it should deform, then apply loads to the actual flap to see how close their hypotheses are.

The Indian education system needs a lot of catching up before it can hope to even perform elementary tests on aircraft sub structures.

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