Galloping Gertie, Engineering's Most Misunderstood Failure (vice.com)
tedlistens writes: Generations of physics teachers, textbooks, and articles have taught that the spectacular collapse of the Tacoma Narrows Bridge, 75 years ago, in November 1940, was caused by resonance. But this explanation is inaccurate, and despite the fact that the collapse is not a mystery—that the bridge, in a sense, twisted itself apart—the fallacy continues to spread. Not only that: according to a new study by Don Olson and colleagues at Texas State University and East Carolina University, parts of the famous footage that immortalized it are misleading too. According to the most complete recent research, he and his co-authors write, "the failure of the bridge was related to a wind-driven amplification of the torsional oscillation that, unlike a resonance, increases monotonically with increasing wind speed." Each time the deck of the bridge twisted now, it sought to return to its original position (inertial forces). And as it did so, twisting back with a matching speed and direction (elastic forces), the wind and the vortices caught it each time, pushing the deck just a little bit more in that direction (aerodynamic forces). With each twist and each twist back, the size of the twisting slightly increased.
Intuitively, this phenomena as described has the feel of what one thinks of given the word 'resonance'. Perhaps 'pseudo-resonance' would be a good term to apply.
John_Chalisque
Hey Texas dumb-shits, "wind-driven amplification of the torsional oscillation..." Sure as hell sounds like resonance to me. Unless they have some other definition.
The proper term for it is aeroelastic flutter. It's a well understood phenomena most famous in jet airplanes but it occurs other places too including apparently this bridge.
Actually it really is not like resonance but more like and anti-damping force. Resonance is when a periodic force is applied to the system and, when the frequency of that force matches the natural vibration frequency of the system, the steady-state response gives a large amplitude response. The key difference is that with resonance the system is in a steady state with a constant amplitude. With "anti-damping" (called aero-elastic flutter in this case) the amplitude of the system increases with each oscillation since you effectively have a negative damping ratio.
Hence there is a clear difference in the motion between resonance and anti-damping which you can determine by studying the motion which the paper seems to have done. It is NOT just a fancy name for a resonance effect: the behaviour is transitory and not steady-state. However this has been known for over a decade now and I'd be surprised if it were still being taught as resonance in introductory physics courses. Certainly for the one I teach I describe it in terms of damping and point out the fallacy of the resonance explanation.
Isn't this conclusion pretty much identical to the findings sixty years ago? It's no surprise that the explanation was oversimplified to "resonance" by the popular press, but to claim that this is an entirely new result misrepresents what engineers learned from the failure.
When it comes down to it, the basic argument is that the phenomena is aeroelastic flutter not resonance, because the driving force is nearly constant.
However, I suspect if you work it all out the change in amplitude of the rotation is proportional to the Fourier transform of the driving force at the natural frequency of the bridge.
Why is that? The nearly constant driving force is not nearly constant.
It is a composition of oscillating forces spanning a range of frequencies. Of all those forces, only the force oscillating at the natural frequency contributes--hence it is proportional to the Fourier transform.
I don't know where you got those definitions from but they are wrong. Aeroelastic flutter is essentially a form of anti-damping force applied to a simple harmonic oscillator and is neither a type of resonance nor the motion itself: you still need an oscillator to experience the anti-damping.
Simple harmonic motion is just the sinusoidal motion in time. To exhibit resonance you actually need a DAMPED harmonic oscillator (otherwise you have infinite amplitude at resonance) and not all damped harmonic oscillators exhibit resonance: only ones where the damping ratio is less than 1/sqrt(2) will show resonance.
Resonance is when an external force drives a damped, harmonic oscillator at a frequency which generates a maximum amplitude response in the steady state. This last part is very important and is why aero-elastic flutter is not resonance. In resonance the amplitude is large but constant, with aeroelastic flutter it grows exponentially and is part of the transient solution of the damped harmonic oscillator. You can also have aeroelastic flutter in a damped system which cannot show resonance.