aeroelastic การใช้

• The X-53 Active Aeroelastic Wing is a NASA effort.
• This aeroelastic divergence can quickly lead to structural failure.
• Direct drive generators and aeroelastic blades for large wind turbines are being researched.
• He has developed theoretical techniques for the aerodynamic and aeroelastic design of the HondaJet.
• NOTE : The Tacoma Narrows actually failed due to Aeroelastic Flutter, not by resonance.
• Vortex shedding was one of the causes proposed for the failure of the original aeroelastic flutter.
• In particular, they show that the aeroelastic wing might actually bend less than a conventional wing.
• In many physics textbooks, the event is presented as an example of elementary forced aeroelastic flutter.
• This is a so-called torsional vibration mode ( which is different from the aeroelastic fluttering.
• A tensioned but flexible belt vibrates by the passing flow of air, due to aeroelastic flutter.
• The Transonic Dynamics Wind Tunnel now used exclusively for aeroelastic research is based on the same principles.
• The X-53 Active Aeroelastic Wing was a US Air Force, Boeing, and NASA effort.
• The X-53 Active Aeroelastic Wing was a US Air Force, NASA, and Boeing effort.
• Small carefully chosen changes to mass distribution and local structural stiffness can be very effective in solving aeroelastic problems.
• Active aeroelastic wing technology is a design approach that enables a higher aspect ratio, more aerodynamically efficient wing.
• The unsteady solver is not only used to simulate gusts, but it is the core of the aeroelastic module.
• Cause was found to be high-frequency, low-amplitude aeroelastic flutter of both the vertical and horizontal stabilizers.
• The NASA version is the X-53 Active Aeroelastic Wing while the United States Air Force tested the Adaptive Compliant Wing.
• Similar aeroelastic tailoring was later applied to experimental forward-swept wings, where it is a necessity for any safe design.
• With the new aeroelastic wing technology, slight deflections of the leading and trailing edge will change the profile of the whole wing.