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Mysterious Sound Waves Can Destroy Rockets

Ponca City, We love you writes "Scientists believe that powerful and unstable sound waves, created by energy supplied by the combustion process, were the cause of rocket failures in several US and Russian rockets. They have also observed these mysterious oscillations in other propulsion and power-generating systems such as missiles and gas turbines. Now, researchers at the Georgia Institute of Technology have developed a liquid rocket engine simulator and imaging techniques to help demystify the cause of these explosive sound waves and bring scientists a little closer to being able to understand and prevent them. The team was able to clearly demonstrate that the phenomenon manifests itself in the form of spinning acoustic waves that gain destructive power as they rotate around the rocket's combustion chamber at a rate of 5,000 revolutions per second. Researchers developed a low-pressure combustor to simulate larger rocket engines then used a very-high-speed camera with fiber optic probes to observe the formation and behavior of excited spinning sound waves within the engine. 'This is a very troublesome phenomenon in rockets,' said Professor Ben Zinn. 'These spinning acoustic oscillations destroy engines without anyone fully understanding how these waves are formed. Visualizing this phenomenon brings us a step closer to understanding it.'"

37 of 193 comments (clear)

  1. Brown noise by rubies · · Score: 5, Funny

    It makes rocket scientists crap their pants!

    1. Re:Brown noise by menkhaura · · Score: 3, Funny

      Bah, rocket science isn't brain surgery!

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    2. Re:Brown noise by definate · · Score: 3, Funny

      Exactly, it's not like it's rocket surgery!

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  2. Good news! by bluephone · · Score: 5, Funny

    This means rocket science is once again hard. You may now resume saying "Well, this isn't rocket science" until they solve this.

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    1. Re:Good news! by fractoid · · Score: 3, Funny

      Bah, this isn't hard. These rockets are just getting speed wobbles, any 8-year-old boy with a bike will be able to tell you all about them!

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    2. Re:Good news! by susano_otter · · Score: 4, Insightful

      This means rocket science is once again hard. You may now resume saying "Well, this isn't rocket science" until they solve this.

      But shockwave instability in rocket propulsion systems has been a known problem since the very beginning of rocketry. They've been solving it repeatedly for decades. Heck, the Saturn V's F1 engine had it bad in early designs. Solving the F1's shockwave problem required significant innovations in testing methods and tools, and in fuel injection techniques, but solved it was.

      The only thing going on today is the same thing that's been going recently in a lot of fields from building architecture to aerodynamics: the replacement of empirical trial-and-error problem-solving methods with highly complex mathematically-driven computer simulation methods.

      Indeed, this advancement of the state of the art will make rocket science easier, since it allows researchers to model different designs in much greater detail, without having to physically build them.
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  3. I've been a member of slashdot for some time by JeanBaptiste · · Score: 5, Funny

    and the subject line for this article has finally convinced me that cowboy neal is in fact art bell.

  4. I can finally be of use to science by Profane+MuthaFucka · · Score: 5, Funny

    I wonder if they'd be interested in analyzing the smoking ruins of at least 5 toilet bowls I have personally destroyed with mysterious oscillating rocket powered sound waves.

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    1. Re:I can finally be of use to science by Tablizer · · Score: 5, Funny

      I wonder if they'd be interested in analyzing the smoking ruins of at least 5 toilet bowls I have personally destroyed with mysterious oscillating rocket powered sound waves.

      Oh great, Mr. Goatse himself is now posting on slashdot.

    2. Re:I can finally be of use to science by NevarMore · · Score: 4, Funny

      Oh great, Mr. Goatse himself is now posting on slashdot.


      Thats impossible. In order to get a good sound out of that it'd have to be a bit tighter and able to make a good PHHHHHHBBBBBTTT sound. The way Mr. Goatse is now it would just kind of go phooooo. Even then I doubt if there is enough of a seal left to keep it from leaking out long enough to build up sufficient volume and pressure to do anything noticable.
    3. Re:I can finally be of use to science by PitaBred · · Score: 5, Funny

      It scares me that you have devoted that much time thinking about the physics of that.

  5. Defense System? by BountyX · · Score: 4, Insightful

    Could be implemented in a way to defend against rocket\missle attacks? Possibly in a better way than Star Wars program.

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    1. Re:Defense System? by zappepcs · · Score: 4, Funny

      Ever watch the movie Dune?

      Moha deeb.... rocket go boom

    2. Re:Defense System? by evanbd · · Score: 4, Insightful

      No. We're talking about pressure waves inside the engine, at pressures measured in tens or hundreds of psi, that resonate with the injector to build power -- think about blowing across the top of a beer bottle. The small power input from your breath induces a higher power oscillation. Same effect, where the bottle is replaced by the combustion chamber and your breath by the injectors. Except the power involved is a hundred million times higher (maybe more, I didn't do the math very carefully).

      These waves can't be set up unless the engine will support them, and if it will then they'll happen on their own. If you could deliver that much energy to the engine remotely, you could just as easily destroy the rocket. It's the *resonance* that's the problem, not the fact that there's a crapload of sound energy available.

    3. Re:Defense System? by evanbd · · Score: 5, Interesting

      The laser beam is way more feasible, even if you ignore considerations of range. Not to mention that when a liquid-fueled military rocket is operating, it's going to be either over the horizon or in vacuum -- we're not talking about small tactical missiles here.

      We're talking about loud sounds here -- and not just a little bit loud. 1 pascal of pressure wave is 94dB SPL -- a fairly loud sound. 1 psi is 6894 pascals; we're talking about many psi of pressure variation. A 10 psi wave would be 190dB. That's not just loud enough to cause hearing damage; that's well past loud enough to knock over buildings. Overpressure from large bombs is less than that at the edge of the blast radius.

      It should be obvious why that's destructive when it happens inside a rocket chamber, especially since oscillations like that tend to start small, grow *rapidly*, and not stop growing until something breaks. It should also be obvious why you won't be able to create such a wave via external influence unless the chamber can already resonate in that mode. When developing the F1 (Saturn V main engine) NASA had trouble with instability; in order to see whether the engine was barely stable or had plenty of margin, they had to find techniques to induce these waves. What they developed, and still use today, is a set of techniques for putting an explosive charge *inside* the engine, bringing the engine up to normal operating conditions (making the charge survive this is nontrivial), and *then* detonating it to see how the engine responded.

  6. Re:Vibrator?? by compro01 · · Score: 5, Funny

    of course. we've got lots of pictures. =D

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  7. If you play them backwards by xs650 · · Score: 4, Funny

    If you record them and play them backwards they will install Vista on your computer.

  8. Summary is a bit off by evanbd · · Score: 5, Informative

    The new result here isn't acoustic instabilities; those have been known for a long time. The interesting result is a new set of imaging techniques that give a better understanding of *why* they occur, rather than simply observing on pressure traces that they *do* occur. After a bit more research, this may turn into techniques to more reliably avoid them in the design stage, rather than having to go through various tweaks on the injector / combustion chamber to remove them should they appear.

    This is very cool work. Of course, it's rocket science, not rocket engineering, so it's unlikely to impact new designs for several years yet.

    1. Re:Summary is a bit off by Nefarious+Wheel · · Score: 3, Interesting
      A problem with dealing with acoustic resonance is just how to manufacture the rocket nozzle to avoid the buildup of these dangerous resonances. Modelling them is the first step, but how can you build the nozzle with sufficient strength while building in structure to interrupt the phase of the wave repeats? Experimentation is a lot cheaper when you can simulate the results. I could imagine moving to non-round shapes might solve the problem, or heterogenious structures - possibly by introduction of dissimilar materials in the bell, perhaps a strapped interspersion of titanium and stainless? I wonder how difficult that could be to model.

      Or I could be full of crap, which is also a distinct possibility.

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    2. Re:Summary is a bit off by evanbd · · Score: 4, Informative

      No, you're on the right track, but not quite there. Computational techniques are only barely able to simulate rocket chambers well; combustion dynamics are complex and not well understood. That's a large part of what makes this work interesting (the other part being the imaging techniques to actually photograph the waves).

      The problem isn't actually the chamber or nozzle walls resonating, it's the acoustic cavity -- exactly analogous to an organ pipe. There are a variety of techniques used to de-tune the resonance modes. (It also happens in the chamber, not the nozzle -- gas in the expansion portion of the nozzle is locally supersonic, so sound can't propagate backwards, which means no resonance.) For example, the SSME has some of the injectors protruding further into the chamber than others, creating interruptions in the flat surface of the injector face. There exist other techniques, and some google searching will turn up some. Also, playing with the metals in the chamber wall is probably right out -- they're basically already decided by thermal considerations, and high performance engines almost universally use copper.

      Historically, the design process has involved experienced engineers, rules of thumb, and lots of testing. Computer models will help, but they'll never really replace the "lots of testing" stage. At least for small engines (up to several thousand pounds of thrust), it's cheaper, easier, and more accurate to just build the thing.

    3. Re:Summary is a bit off by jake-in-a-box · · Score: 3, Informative

      I think you answered your own question. Copper is the best conductor of the materials you mentioned. The engines are cooled by circulating the fuel around them prior to its introduction into the combustion chamber. Heat conduction is analogous to electrical conduction, so copper is probably the best combination of inherent strength and heat conduction available. Still probably alloyed because pure copper is soft.

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    4. Re:Summary is a bit off by evanbd · · Score: 5, Informative

      Titanium may melt at 1900K, but rocket chambers operate in the realm of 2500-3500K. They have to be cooled, and copper is the material of choice for the same reason it makes good CPU heat sinks -- excellent thermal conductivity. Some older thrust chambers were made of steel (WAC Corporal, iirc), and it works at low chamber pressures (less heat flux), but it doesn't work as well and there are corrosion issues in storage. As performance increases and chamber pressures rise, metals other than copper look less and less appealing.

      Some nozzles are uncooled in the aft portion (as the gas expands and accelerates, it cools down, so the environment gets easier to handle). The Kestrel engine used in the Falcon 1 upper stage, for example, has a radiatively cooled Niobium nozzle. Titanium has been used, but Niobium and a few others tend to perform better in that environment -- the combination of hot reactive gases is hard to handle.

  9. This has got to be joke by Riktov · · Score: 4, Funny

    Come on, an expert on rocket fuel technology named Professor Ben Zinn?

  10. Powerful sound waves? by gmuslera · · Score: 3, Funny

    Heavy Metal can destroy even rockets now.

  11. Turn it inside out. by camperdave · · Score: 5, Interesting

    Rocket engines typically have a round cross section, which, if it doesn't aid the production of these circular waves, probably does little to dampen them. I wonder if the "inside out" design of a linear aerospike engine suffers from the same problem.

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    1. Re:Turn it inside out. by evanbd · · Score: 3, Interesting

      Aerospike engines still have an enclosed chamber; it's only the nozzle that's been changed. The chamber is where the problems occur, not the nozzle. The odd chamber shapes certainly make things complicated, but I have no idea whether they hurt or help overall. The usual technique to get rid of these involves various ways to de-tune the engine -- for example, some of the SSME injectors protrude deeper into the chamber to interrupt the otherwise flat injector face.

    2. Re:Turn it inside out. by icebrain · · Score: 3, Informative

      It does depict them, you just aren't looking hard enough. On a traditonal rocket engine, the chamber is a bulbed or cylindrical chamber above the nozzle. It narrows down, then expands into a bell shape to allow the combusted hot gasses to expand and accelerate.

      http://en.wikipedia.org/wiki/Image:Aerospikeprinciplediagram.gif

      In the linked illustration on the right, look along the top edge of the aerospike, where the flames are coming from. All of the little canisters along both edges (where the flames come out) are combustion chambers. You just have a bunch of small ones instead of one large one. Compare that to the image on the left (a standard bell nozzle)--notice that you have a chamber at the top, which narrows down to a throat, and then opens back up. Basically, an aerospike does is cut off at the throat and turn the nozzle inside out. You then have an inner wall to expand against, with the outside atmosphere providing the outer wal.

      Read this site for more: http://www.aerospaceweb.org/design/aerospike/main.shtml

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  12. Pogo Oscillations by orospakr · · Score: 4, Interesting

    This phenomenon sounds very similar to Pogo Oscillations, which incidentally caused the engine 5 shutdown on the Apollo 13 Saturn V.

      http://en.wikipedia.org/wiki/Pogo_oscillations

    1. Re:Pogo Oscillations by evanbd · · Score: 3, Informative

      Similar, but different. Both are oscillations, but pogo is characterized by low frequency variations in chamber pressure coupling through the thrust structure and into the propellant feed system (and from there back to the chamber pressure). These are high frequency (kHz, no tens of Hz) acoustic modes, contained entirely within the chamber. They're much harder simulate and much harder to get rid of, and much less well understood. They couple from local chamber pressure to the injectors, and operate much like an organ pipe.

  13. Addicted to bass... by roxtafari · · Score: 3, Funny

    Looks like an audio engineering issue. While not being a rocket engineer myself, I assume the combustion chamber is somewhat symmetrical. It is likely acting as a resonance chamber and increasing the amplitude of the soundwave to the point of physical damage. I shattered the rear window in my '96 Camaro twice with a 1200W Fosgate and a single 10" bazooka tube. Tell NASA to crack the window when they turn up the bass!

  14. Sonic Tools by Professr3 · · Score: 3, Funny

    So THAT'S how the Doctor's screwdriver works...

  15. Re:"Strange wave phenomenon" = resonance by evanbd · · Score: 3, Informative

    Pogo, pump-related oscillations, and plumbing related oscillations are all low frequency (tens of Hz, sometimes less). These are acoustic modes internal to the chamber, in the kHz range. They're very distinct phenomenon, with distinct causes and distinct solutions. They're still a 50 year old problem with 50 year old techniques to solve them, but they're by no means understood in any meaningful sense -- the current technique mostly involves testing the engine and then tweaking it until they go away.

    The new and interesting work here is the modelling, combined with the photography techniques. Seeing pressure waves at the injector face through the chamber full of flame is not trivial.

  16. Re:Vibrator?? by AmigaHeretic · · Score: 4, Funny

    >>>> Do you even know what a woman looks like?

    >>of course. we've got lots of pictures. =D

    Yeah, and I know all about womens emotions and stuff. Like, chicks HATE it when you call them broads.

  17. Combustion instability is an old problem by Animats · · Score: 3, Interesting

    Combustion instability is an old problem with rocket engines. The Saturn V main engine had serious combustion instability problems, which were fixed by trial and error testing. The Apollo booster people had to resort to setting off small bombs inside engines on test stands to induce instability, then trying different patterns of holes in the plates the distributed fuel to find a stable configuration.

    The SR-71 engine had serious combustion instability. That, too, was fixed with something of a hack, an automated "sympathetic unstart" system which, when one engine had a stall, would stall the other one, then restart both.

    Better simulation tools in that area can't hurt. Not many big supersonic engines are designed any more. As Scott Crossfield pointed out just before he died a few years ago, every aircraft that went significantly over Mach 3 is now in a museum.

  18. Somthing Wrong Here. was Re:Nothing new here by FlyingGuy · · Score: 5, Informative

    Ok, before parent gets any farther this has to be de-bunked. Sound waves did not destroy the bridge. A sound wave, in any medium consists of a compression and a rarifraction ., that is a leading pressure wave followed by a area of lower pressure that propagate in a known fashion. The intensity of a sound wave obeys the inverse square law.

    What happened to the Tacoma Narrows Bride was caused be an error in aerodynamic calculations on the part of the design engineer. Air passing around the bridge deck acted exactly like air does when presented with a crude airfoil, it formed an area of low pressure leeward of the bridge deck and a low pressure area leeward and below the bridge deck. Th resulting high pressure and low pressure vectors imparted a twisting moment to the bridge deck.

    The twisting moment was resisted by the torsional rigidity of the bridge deck. This caused the deck to twist to and build torsional tension. The twisting caused the aerodynamic profile of the bridge deck to change. The resulting change allowed the bridge deck to revert back to its original shape and aerodynamic profile, rinse and repeat. Thus the repeated twisting caused enough of the riveted and bolted joints to fail which led to a cascade failure as the remaining joints failed under the bridges weight and twisting motion.

    This was not "low frequency sound waves" although the structures oscillations did cause some very low frequency sounds waves, it was destroyed by nothing more then bad aerodynamics.

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  19. Coriolis Effect in Vortex Combustion by Baldrson · · Score: 4, Interesting

    This racetrack instability is actually a well known problem with annular combustion chambers such as those used with the toroidal aerospike engine. One of the main virtues of vortex engines, like Orbital Technologies or the ultracentrifugal one invented by Roger Gregory and myself, is that the coriolis effect distorts the wave front sending it into the wall of the combustion chamber. In theory, at least, this should disrupt the resonance enough to prevent destructive standing waves. Experiments have not been conducted to test this theory yet to the best of my knowledge.

  20. Re:Harmonics by IndustrialComplex · · Score: 3, Interesting

    Once the dB level of sound starts to approach that which is experienced in the engine of a rocket, it isn't even resonance anymore, it's just plain extreme force.

    It generally takes about 110dB to shatter a wine glass via oscillation, but it isn't direct exposure to the pressure that causes that.

    Depending on the quality, glass will begin to shatter above 160-165 dB, independant of its resonant frequency. Of course, if you are dealing with flexible glass, that value will increase.

    It is quite possible to have a sound wave impact with enough force on a specific area in a rocket engine to cause enough fatigue which will result in a failure without actually resonating.

    So why is this news? Because depending on the atmospheric pressure, once you get above 194 dB, the soundwave becomes distorted, it would be difficult enough to model a soundwave in a motionless, inactive engine, but I can't even begin to comprehend how complex the modeling must be of an engine that is generating sound waves in excess of 200dB in such an extreme and dynamic environment.

    That they are able to model this is amazing.

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