1 00:00:06,230 --> 00:00:04,150 on most days we get a chance to see the 2 00:00:09,030 --> 00:00:06,240 international space station crew members 3 00:00:11,350 --> 00:00:09,040 working on science experiments 4 00:00:14,150 --> 00:00:11,360 sometimes we get to see the experiments 5 00:00:16,470 --> 00:00:14,160 themselves as they do their thing 6 00:00:18,950 --> 00:00:16,480 recently the international space station 7 00:00:21,750 --> 00:00:18,960 program science office posted a video 8 00:00:23,349 --> 00:00:21,760 clip on the real nasa youtube channel 9 00:00:24,950 --> 00:00:23,359 from a combustion experiment that's 10 00:00:26,550 --> 00:00:24,960 underway and that clip has caught an 11 00:00:33,510 --> 00:00:26,560 awful lot of attention 12 00:00:39,030 --> 00:00:35,830 that's from the flame extinguishment 13 00:00:41,190 --> 00:00:39,040 experiment 2 or flex 2. 14 00:00:43,750 --> 00:00:41,200 earlier this week i spoke with dr tom 15 00:00:46,549 --> 00:00:43,760 avedisian of cornell university who is 16 00:00:48,549 --> 00:00:46,559 the flex 2 co-investigator who requested 17 00:00:51,029 --> 00:00:48,559 that particular test burn 18 00:00:53,430 --> 00:00:51,039 to find out what it is we're seeing here 19 00:00:55,750 --> 00:00:53,440 and what scientists are trying to learn 20 00:00:58,310 --> 00:00:55,760 from burning things in space 21 00:01:00,310 --> 00:00:58,320 well our overarching objectives are to 22 00:01:03,270 --> 00:01:00,320 obtain information about how liquid 23 00:01:05,030 --> 00:01:03,280 fuels burn so we can design ultimately 24 00:01:08,550 --> 00:01:05,040 more efficient combustion engines used 25 00:01:10,630 --> 00:01:08,560 in transportation systems on earth 26 00:01:12,870 --> 00:01:10,640 the the problem with that is that real 27 00:01:15,270 --> 00:01:12,880 liquid fuels like gasoline diesel and 28 00:01:17,109 --> 00:01:15,280 jet fuel are so complex 29 00:01:20,070 --> 00:01:17,119 that it's really a hopeless task to 30 00:01:21,670 --> 00:01:20,080 develop models for how they burn as they 31 00:01:24,070 --> 00:01:21,680 contain hundreds of miscible 32 00:01:27,429 --> 00:01:24,080 constituents with a wide range of 33 00:01:29,190 --> 00:01:27,439 boiling points propensities to form soot 34 00:01:31,270 --> 00:01:29,200 during combustion 35 00:01:33,749 --> 00:01:31,280 and heats of vaporization soot is the 36 00:01:34,469 --> 00:01:33,759 black carbonaceous material we sometimes 37 00:01:36,550 --> 00:01:34,479 see 38 00:01:38,390 --> 00:01:36,560 spew out the dispute out of the exhaust 39 00:01:40,390 --> 00:01:38,400 line of diesel trucks which is 40 00:01:41,510 --> 00:01:40,400 responsible for a whole host of health 41 00:01:43,830 --> 00:01:41,520 risks 42 00:01:45,510 --> 00:01:43,840 where we are addressing this problem our 43 00:01:48,950 --> 00:01:45,520 approach by studying the combustion 44 00:01:51,830 --> 00:01:48,960 dynamics of fuel blends comprised of a 45 00:01:54,789 --> 00:01:51,840 much smaller number of constituents say 46 00:01:56,469 --> 00:01:54,799 for example two or three ideally 47 00:01:58,709 --> 00:01:56,479 with the hope that they will replicate 48 00:01:59,749 --> 00:01:58,719 certain combustion targets of the real 49 00:02:01,749 --> 00:01:59,759 fuel 50 00:02:04,230 --> 00:02:01,759 we would then develop the understanding 51 00:02:06,389 --> 00:02:04,240 of that simpler blend which we call a 52 00:02:08,550 --> 00:02:06,399 surrogate and use the combustion 53 00:02:10,869 --> 00:02:08,560 properties of the surrogate to assess 54 00:02:13,910 --> 00:02:10,879 the performance of the real fuel 55 00:02:16,710 --> 00:02:13,920 now in fact you're doing the these uh 56 00:02:18,949 --> 00:02:16,720 experiments in space by burning just 57 00:02:20,949 --> 00:02:18,959 single droplets of fuel right tell me 58 00:02:23,750 --> 00:02:20,959 why that why you do it that way 59 00:02:25,270 --> 00:02:23,760 well that that's that's correct our our 60 00:02:27,430 --> 00:02:25,280 strategy has been developed the 61 00:02:30,390 --> 00:02:27,440 combustion properties for evaluating a 62 00:02:32,869 --> 00:02:30,400 surrogate by using the simplest possible 63 00:02:36,390 --> 00:02:32,879 configuration of burning for a liquid 64 00:02:38,790 --> 00:02:36,400 fuel namely a droplet burning under 65 00:02:41,670 --> 00:02:38,800 conditions that promote spherically 66 00:02:43,750 --> 00:02:41,680 symmetric gas transport this kind of 67 00:02:45,990 --> 00:02:43,760 combustion symmetry is currently the 68 00:02:48,309 --> 00:02:46,000 only one for a liquid fuel that can be 69 00:02:51,350 --> 00:02:48,319 modeled using detailed 70 00:02:53,350 --> 00:02:51,360 simulation or first principles approach 71 00:02:55,350 --> 00:02:53,360 where no sub models or adjustable 72 00:02:57,589 --> 00:02:55,360 constants are required 73 00:03:00,309 --> 00:02:57,599 this is precisely what is needed to 74 00:03:03,110 --> 00:03:00,319 evaluate the efficacy of a surrogate to 75 00:03:05,670 --> 00:03:03,120 perform like a real fuel it is intended 76 00:03:08,149 --> 00:03:05,680 to replicate and in space you get to do 77 00:03:10,390 --> 00:03:08,159 these experiments inside an apparatus 78 00:03:12,949 --> 00:03:10,400 called the multi-use droplet combustion 79 00:03:16,550 --> 00:03:12,959 apparatus that allows you to control 80 00:03:17,670 --> 00:03:16,560 variables right that is correct the mdca 81 00:03:20,390 --> 00:03:17,680 as its 82 00:03:23,750 --> 00:03:20,400 shorthand notation has the capability to 83 00:03:25,830 --> 00:03:23,760 control the droplet size which is a very 84 00:03:28,229 --> 00:03:25,840 important parameter that influences soot 85 00:03:30,630 --> 00:03:28,239 formation and radiative losses 86 00:03:32,390 --> 00:03:30,640 as well as the ambient oxygen and inner 87 00:03:34,070 --> 00:03:32,400 gas concentration 88 00:03:35,270 --> 00:03:34,080 and pressure up to about three 89 00:03:38,710 --> 00:03:35,280 atmospheres 90 00:03:40,550 --> 00:03:38,720 currently we do experiments my component 91 00:03:43,030 --> 00:03:40,560 of the flex project is essentially at 92 00:03:45,110 --> 00:03:43,040 room temperature air 93 00:03:47,190 --> 00:03:45,120 obviously the facility includes storage 94 00:03:49,030 --> 00:03:47,200 chambers for a range of fuels with the 95 00:03:51,350 --> 00:03:49,040 ones we are investigating being 96 00:03:53,190 --> 00:03:51,360 representative of components of real 97 00:03:55,750 --> 00:03:53,200 transportation fuels 98 00:03:58,309 --> 00:03:55,760 now we mentioned earlier that there's a 99 00:04:00,550 --> 00:03:58,319 a video on youtube that shows kind of a 100 00:04:03,270 --> 00:04:00,560 remarkable burn and i'd like to play 101 00:04:05,990 --> 00:04:03,280 that again and have you described for me 102 00:04:07,190 --> 00:04:06,000 what it is that we see in this video 103 00:04:09,830 --> 00:04:07,200 okay 104 00:04:11,830 --> 00:04:09,840 um it's a very delicate operation 105 00:04:14,470 --> 00:04:11,840 there's a zooming out and you'll see 106 00:04:15,910 --> 00:04:14,480 very quickly the the activation and the 107 00:04:17,909 --> 00:04:15,920 ignition event 108 00:04:20,150 --> 00:04:17,919 the droplet looks motionless but 109 00:04:22,150 --> 00:04:20,160 actually it is moving a little bit 110 00:04:24,790 --> 00:04:22,160 and you'll see in the lower left-hand 111 00:04:26,070 --> 00:04:24,800 corner the flame disappearing and then 112 00:04:28,629 --> 00:04:26,080 reappearing 113 00:04:31,270 --> 00:04:28,639 and we believe that this is the result 114 00:04:34,390 --> 00:04:31,280 of movement of the droplet such that 115 00:04:37,670 --> 00:04:34,400 when the droplet is moving fresh oxygen 116 00:04:39,990 --> 00:04:37,680 is drawn into the combustion zone but it 117 00:04:41,909 --> 00:04:40,000 also depletes the oxygen on the back 118 00:04:44,070 --> 00:04:41,919 side of the droplet which causes 119 00:04:47,030 --> 00:04:44,080 extinction but that movement of the 120 00:04:50,150 --> 00:04:47,040 droplet allows the flame to close on the 121 00:04:52,469 --> 00:04:50,160 backside the continued movement it opens 122 00:04:55,110 --> 00:04:52,479 up again and you can execute multiple 123 00:04:57,350 --> 00:04:55,120 cycles of this what appears like a 124 00:04:59,189 --> 00:04:57,360 jellyfish type of motion 125 00:05:01,830 --> 00:04:59,199 i mean we don't really know 126 00:05:03,909 --> 00:05:01,840 the the detailed mechanism for this this 127 00:05:05,830 --> 00:05:03,919 is purely speculation on our part but 128 00:05:07,670 --> 00:05:05,840 this is what we think is happening 129 00:05:09,189 --> 00:05:07,680 but as you explained earlier one of the 130 00:05:11,350 --> 00:05:09,199 things that you're looking at is what 131 00:05:13,670 --> 00:05:11,360 happens to the soot during these burns 132 00:05:16,070 --> 00:05:13,680 and you really can't see that in that 133 00:05:17,830 --> 00:05:16,080 video but you provided us with another 134 00:05:19,670 --> 00:05:17,840 uh video clip 135 00:05:22,790 --> 00:05:19,680 from a black and white camera in the 136 00:05:25,350 --> 00:05:22,800 mdca i want to show that because it also 137 00:05:27,110 --> 00:05:25,360 has some pretty remarkable movement in 138 00:05:28,070 --> 00:05:27,120 there and get you to describe what we're 139 00:05:31,029 --> 00:05:28,080 seeing 140 00:05:34,550 --> 00:05:31,039 well this video is of a toluene fuel 141 00:05:36,310 --> 00:05:34,560 toluene is a constituent of uh gasoline 142 00:05:39,990 --> 00:05:36,320 here you see as soon as the ignition 143 00:05:42,710 --> 00:05:40,000 process occurs soot explodes into view 144 00:05:44,790 --> 00:05:42,720 and as you noted this is a backlit image 145 00:05:47,270 --> 00:05:44,800 so we see the dropper that's the black 146 00:05:50,150 --> 00:05:47,280 ball that's kind of very slowly drifting 147 00:05:51,749 --> 00:05:50,160 and the soot particles are almost in the 148 00:05:54,950 --> 00:05:51,759 state of left um 149 00:05:56,870 --> 00:05:54,960 animated levitation around the droplet 150 00:05:58,550 --> 00:05:56,880 the flame is actually extinguished but 151 00:06:01,029 --> 00:05:58,560 you can't see it here 152 00:06:03,590 --> 00:06:01,039 um the droplet is drifting but the soot 153 00:06:06,469 --> 00:06:03,600 particles remain somewhat in place that 154 00:06:08,710 --> 00:06:06,479 is a remarkable illustration of the 155 00:06:11,670 --> 00:06:08,720 formation of soot under the spherically 156 00:06:13,670 --> 00:06:11,680 symmetric condition it's remarkable even 157 00:06:15,510 --> 00:06:13,680 for for the layman to look at that and 158 00:06:17,670 --> 00:06:15,520 and to have just a beginning of an 159 00:06:19,510 --> 00:06:17,680 understanding of what we're seeing there 160 00:06:21,590 --> 00:06:19,520 can you explain to us 161 00:06:24,390 --> 00:06:21,600 how you imagine the results what you're 162 00:06:25,590 --> 00:06:24,400 getting in these burns how they can be 163 00:06:27,909 --> 00:06:25,600 applicable 164 00:06:30,390 --> 00:06:27,919 for in future uses 165 00:06:32,309 --> 00:06:30,400 well as i as i remarked earlier we have 166 00:06:35,189 --> 00:06:32,319 been using the multi-user droplet 167 00:06:37,909 --> 00:06:35,199 combustion apparatus on on the space 168 00:06:40,390 --> 00:06:37,919 station to study how surrogates for real 169 00:06:43,270 --> 00:06:40,400 liquid transportation fuels burn when 170 00:06:44,469 --> 00:06:43,280 subjected to the idealized environment 171 00:06:46,790 --> 00:06:44,479 of 172 00:06:48,390 --> 00:06:46,800 no convection and no relative droplet 173 00:06:50,230 --> 00:06:48,400 gas velocity that's going to create 174 00:06:53,110 --> 00:06:50,240 spherical drop of flames 175 00:06:54,870 --> 00:06:53,120 we feel there are few configurations 176 00:06:57,270 --> 00:06:54,880 better suited to get this type of 177 00:06:58,870 --> 00:06:57,280 understanding i would also note 178 00:07:01,029 --> 00:06:58,880 or like to note that with the new 179 00:07:03,350 --> 00:07:01,039 generation of fuels emerging that will 180 00:07:05,830 --> 00:07:03,360 be derived from a wide range of biofeed 181 00:07:08,390 --> 00:07:05,840 stocks like algae camelina soybean and 182 00:07:10,150 --> 00:07:08,400 so forth the mdca 183 00:07:12,150 --> 00:07:10,160 with the spherically symmetric burning 184 00:07:14,629 --> 00:07:12,160 process it can promote is i think well 185 00:07:16,550 --> 00:07:14,639 positioned to reveal the influence of 186 00:07:19,110 --> 00:07:16,560 fuel composition and droplet size 187 00:07:21,350 --> 00:07:19,120 effects on ignition combustion kinetic 188 00:07:23,110 --> 00:07:21,360 measurement 189 00:07:25,830 --> 00:07:23,120 combustion kinetic mechanisms and so 190 00:07:28,150 --> 00:07:25,840 forth that control burning developing 191 00:07:30,870 --> 00:07:28,160 surrogates for these biofuels 192 00:07:32,790 --> 00:07:30,880 is essential to access this information 193 00:07:35,189 --> 00:07:32,800 and and armed with it 194 00:07:37,909 --> 00:07:35,199 uh the combustion chemistry for these 195 00:07:41,110 --> 00:07:37,919 simpler brands uh other characteristics 196 00:07:43,430 --> 00:07:41,120 of biofuels uh can be obtained uh that 197 00:07:45,670 --> 00:07:43,440 should ultimately uh allow us to predict 198 00:07:47,749 --> 00:07:45,680 their performance in combustion engines 199 00:07:49,909 --> 00:07:47,759 for this new generation of fuels 200 00:07:51,749 --> 00:07:49,919 be very interesting to keep track of 201 00:07:53,749 --> 00:07:51,759 this as it goes forward and see how it 202 00:07:56,950 --> 00:07:53,759 works i appreciate you taking the time 203 00:07:59,670 --> 00:07:56,960 to explain it to us thank you very much 204 00:08:02,230 --> 00:07:59,680 dr tom avedisian of cornell university 205 00:08:03,749 --> 00:08:02,240 is a co-investigator of the flex 2