WEBVTT 00:00:01.268 --> 00:00:03.111 - Let's talk about the Venturi effect. 00:00:03.111 --> 00:00:05.688 This has to do with water or any fluid 00:00:05.688 --> 00:00:07.360 flowing through a pipe. 00:00:07.360 --> 00:00:10.263 And it turns out, let's say this water's flowing right here. 00:00:10.263 --> 00:00:13.744 Minding its own business, having a good day for that matter, 00:00:13.744 --> 00:00:16.128 when it meets a constriction. 00:00:16.128 --> 00:00:17.591 What's gonna happen here? 00:00:17.591 --> 00:00:19.359 Well, the water's gotta keep flowing, 00:00:19.359 --> 00:00:22.079 but it's gonna start flowing faster 00:00:22.079 --> 00:00:23.632 through the constricted region. 00:00:23.632 --> 00:00:26.151 And the reason is, well, there's a certain amount of 00:00:26.151 --> 00:00:28.103 fluid that's flowing through this pipe. 00:00:28.103 --> 00:00:32.023 Let's say all the fluid in this region right here. 00:00:32.023 --> 00:00:34.401 Let's say this front part of the water. 00:00:34.401 --> 00:00:35.615 I mean, this whole thing's filled up, 00:00:35.615 --> 00:00:38.614 but just say this cross-section of the water 00:00:38.614 --> 00:00:40.966 happened to make it from this back portion 00:00:40.966 --> 00:00:43.751 to this front portion in, I don't know, 00:00:43.751 --> 00:00:45.327 let's just say one second. 00:00:45.327 --> 00:00:49.583 So this entire volume moved through this section 00:00:49.583 --> 00:00:51.254 of the pipe in one second. 00:00:51.254 --> 00:00:54.677 Well, there's a law in physics that says that same volume's 00:00:54.677 --> 00:00:57.647 gotta make it through each portion of this pipe. 00:00:57.647 --> 00:01:00.596 Because if it didn't, where's it gonna go? 00:01:00.596 --> 00:01:02.412 This pipe would have to break or something. 00:01:02.412 --> 00:01:04.077 This water's gotta go somewhere. 00:01:04.077 --> 00:01:06.724 If that much flowed through here in one second, 00:01:06.724 --> 00:01:08.509 then this much has to flow through this 00:01:08.509 --> 00:01:12.101 little tiny region in one second, 00:01:12.101 --> 00:01:15.101 but the only way that that's possible is for this 00:01:15.101 --> 00:01:16.981 front surface, instead of just traveling from 00:01:16.981 --> 00:01:20.573 there to there in one second, the front surface 00:01:20.589 --> 00:01:21.807 is gonna have to change it's shape. 00:01:21.807 --> 00:01:23.351 But the front part of the water's gonna have to 00:01:23.351 --> 00:01:26.534 travel from here to here maybe in 1/4 of a second 00:01:26.534 --> 00:01:29.191 because all of this has gotta cram through here 00:01:29.191 --> 00:01:30.551 in the same amount of time. 00:01:30.551 --> 00:01:31.927 Because that water's still coming behind it. 00:01:31.927 --> 00:01:33.263 There's more water coming. 00:01:33.263 --> 00:01:36.351 And the volume flow rate has got to stay the same. 00:01:36.351 --> 00:01:39.063 The volume per time flowing through one region 00:01:39.063 --> 00:01:41.087 of the pipe has got to be the same as 00:01:41.087 --> 00:01:44.719 the volume flow rate through some other region of the pipe 00:01:44.719 --> 00:01:46.894 because this water's got to go somewhere. 00:01:46.894 --> 00:01:48.799 It doesn't just disappear in here. 00:01:48.799 --> 00:01:50.286 It's gotta keep flowing. 00:01:50.286 --> 00:01:51.662 That means... 00:01:51.662 --> 00:01:54.823 The important part is the water flows faster 00:01:54.823 --> 00:01:56.606 through the constricted region. 00:01:56.606 --> 00:02:00.381 Sometimes much faster through the constricted region. 00:02:00.381 --> 00:02:03.679 The smaller this is compared to this original radius, 00:02:03.679 --> 00:02:06.350 the faster the fluid will flow through here. 00:02:06.350 --> 00:02:07.654 Why do we care? 00:02:07.654 --> 00:02:12.654 Well, because faster moving fluid also means lower pressure. 00:02:13.757 --> 00:02:16.575 Why does faster moving fluid mean lower pressure? 00:02:16.575 --> 00:02:18.253 Well, if we look at the Bernoulli equation, 00:02:18.253 --> 00:02:23.253 Bernoulli's equation says P one plus row g h one 00:02:24.614 --> 00:02:29.470 plus 1/2 row v one squared 00:02:29.470 --> 00:02:34.470 equals P two plus row g h two 00:02:34.685 --> 00:02:38.605 plus 1/2 row v two squared. 00:02:38.605 --> 00:02:40.710 Oh my goodness this looks frightening, 00:02:40.710 --> 00:02:43.718 but look at P one, we just pick some point in the pipe. 00:02:43.718 --> 00:02:45.752 Let's just pick this point right here. 00:02:45.752 --> 00:02:47.446 We'll call that point one. 00:02:47.446 --> 00:02:50.845 So all these ones, this whole side refers to that point. 00:02:50.845 --> 00:02:53.637 Let's just pick point two right here. 00:02:53.637 --> 00:02:55.277 All this whole side refers to that point. 00:02:55.277 --> 00:02:56.077 Now, notice something. 00:02:56.077 --> 00:02:59.349 These are basically the same height, 00:02:59.909 --> 00:03:02.089 and assume height's not really a big difference here. 00:03:02.089 --> 00:03:03.961 So let's cross out the heights, 00:03:03.961 --> 00:03:05.097 because they're the same heights. 00:03:05.097 --> 00:03:06.624 We don't have to worry about that. 00:03:06.624 --> 00:03:10.208 This says that, alright, if there's some pressure at one 00:03:10.208 --> 00:03:12.991 and some velocity of the water at one, 00:03:12.991 --> 00:03:15.103 you can plug those in here and get this side. 00:03:15.103 --> 00:03:15.944 And now look at over here. 00:03:15.944 --> 00:03:18.748 We know that the velocity at two is bigger. 00:03:18.748 --> 00:03:20.372 We just said that, it has to be because the 00:03:20.372 --> 00:03:22.148 volume flow rate's got to stay the same. 00:03:22.148 --> 00:03:24.683 So this speeds up in here. 00:03:24.683 --> 00:03:27.443 So this is bigger, this quantity here. 00:03:27.443 --> 00:03:30.515 But we know the whole thing equals this side. 00:03:30.515 --> 00:03:33.756 So if this term increased, that means that the pressure's 00:03:33.756 --> 00:03:36.524 got to decrease so that when they add up 00:03:36.524 --> 00:03:38.843 they get the same as this side over here. 00:03:38.843 --> 00:03:41.129 This is actually called Bernoulli's Principle. 00:03:41.129 --> 00:03:43.187 Bernoulli's Principle says that when a fluid 00:03:43.187 --> 00:03:45.724 speeds up, it's pressure goes down. 00:03:45.724 --> 00:03:47.892 It's totally counter-intuitive. 00:03:47.892 --> 00:03:49.600 We always expect the opposite. 00:03:49.600 --> 00:03:52.319 We think fast moving fluid, that's gotta 00:03:52.319 --> 00:03:55.871 have a lot of pressure, but it's the exact opposite. 00:03:55.871 --> 00:03:59.455 Fast moving fluid actually has a smaller pressure 00:03:59.455 --> 00:04:01.335 and it's due to Bernoulli's equation. 00:04:01.335 --> 00:04:03.631 And this is what causes the Venturi effect. 00:04:03.631 --> 00:04:05.887 The Venturi effect refers to the fact that if you 00:04:05.887 --> 00:04:08.984 have a tube and you want a smaller pressure region, 00:04:08.984 --> 00:04:10.990 you want the pressure to drop for some reason, 00:04:10.990 --> 00:04:13.615 which actually comes up in a lot of cases, 00:04:13.615 --> 00:04:16.190 just cause a narrow constriction in that tube. 00:04:16.190 --> 00:04:19.945 In this narrow constriction, faster moving fluid, 00:04:19.945 --> 00:04:21.583 and it'll cause a lower pressure. 00:04:21.583 --> 00:04:24.478 This is the idea behind the Venturi effect. 00:04:24.478 --> 00:04:26.599 So the Venturi effect basically says for 00:04:26.599 --> 00:04:30.246 a constriction in a pipe, you're gonna get a lower pressure. 00:04:30.246 --> 00:04:32.239 While we're talking about fluid flow, 00:04:32.239 --> 00:04:34.491 we should talk about one more thing. 00:04:34.491 --> 00:04:36.811 Let me get rid of this here. 00:04:36.811 --> 00:04:38.747 Imagine you just had a brick wall 00:04:38.747 --> 00:04:40.587 with fluid flowing towards it. 00:04:40.587 --> 00:04:41.779 Maybe it's air here. 00:04:41.779 --> 00:04:45.885 So you've got some fluid flowing towards this brick wall. 00:04:45.885 --> 00:04:47.906 This seems like a really dumb example of 00:04:47.906 --> 00:04:49.851 Bernoulli's principle but I'm going somewhere 00:04:49.851 --> 00:04:51.858 with this so stay with me. 00:04:51.858 --> 00:04:53.074 This is flowing towards here. 00:04:53.074 --> 00:04:54.153 What's going to happen? 00:04:54.153 --> 00:04:56.106 Well, it can't go through the wall. 00:04:56.106 --> 00:04:57.346 It's gotta go somewhere. 00:04:57.346 --> 00:05:00.322 Maybe this just goes up like that 00:05:00.322 --> 00:05:02.345 and this, you know, I'm gonna go this way. 00:05:02.345 --> 00:05:04.155 It's closer to go that way. 00:05:04.155 --> 00:05:05.907 This side maybe just goes down. 00:05:05.907 --> 00:05:07.946 This is actually kind of what happens. 00:05:07.946 --> 00:05:09.618 But there'll be a portion in the middle 00:05:09.618 --> 00:05:11.121 that basically just terminates. 00:05:11.121 --> 00:05:14.417 It hits here and kind of just gets stuck. 00:05:14.417 --> 00:05:17.167 So there'll be some air right near here in the middle 00:05:17.167 --> 00:05:19.221 where it's just not moving. 00:05:19.221 --> 00:05:20.638 What if we wanted to know what the pressure 00:05:20.638 --> 00:05:24.333 was there, based on the variables involved in this problem? 00:05:24.333 --> 00:05:26.882 We could use Bernoulli's equation again. 00:05:26.882 --> 00:05:30.109 Pick two points, let's pick this one, point one. 00:05:30.109 --> 00:05:32.682 Let's pick this one, point two. 00:05:32.682 --> 00:05:35.917 Use Bernoulli's equation, it says this, 00:05:35.917 --> 00:05:39.597 and again let's say these are basically the same height 00:05:39.597 --> 00:05:41.901 so that height is not a big factor. 00:05:41.901 --> 00:05:43.746 And if these terms are the same, 00:05:43.746 --> 00:05:45.502 then we can just cross them out because we can 00:05:45.502 --> 00:05:48.723 subtract them from both sides, they're identical. 00:05:48.723 --> 00:05:50.139 Now, what can we say? 00:05:50.139 --> 00:05:52.924 We know the velocity of the air at two. 00:05:52.924 --> 00:05:54.724 It's not moving, got stuck here. 00:05:54.724 --> 00:05:55.908 It got stagnant. 00:05:55.908 --> 00:05:58.436 And so v two is just zero. 00:05:58.436 --> 00:06:00.659 And we get this statement that the pressure 00:06:00.659 --> 00:06:05.659 at two, which is sometimes called the stagnation pressure, 00:06:06.137 --> 00:06:08.714 so I'm gonna call it the stagnation pressure, 00:06:08.714 --> 00:06:12.267 because the air right here gets stuck and it's not moving. 00:06:12.267 --> 00:06:14.818 You might object, you might say, "Wait, hold on. 00:06:14.818 --> 00:06:16.523 "I thought the air had to go somewhere?" 00:06:16.523 --> 00:06:17.930 Well, it's all going somewhere. 00:06:17.930 --> 00:06:22.378 The point is, there's some air right here that gets stuck. 00:06:22.378 --> 00:06:25.442 It get stuck and air starts passing it by. 00:06:25.442 --> 00:06:27.354 And so, what's this pressure here? 00:06:27.354 --> 00:06:28.714 Well, up here we just read it off. 00:06:28.714 --> 00:06:30.226 All these went away. 00:06:30.226 --> 00:06:33.306 P two, which is what I'm calling the stagnation pressure, 00:06:33.306 --> 00:06:37.913 has gotta equal P one, the pressure over here, 00:06:37.913 --> 00:06:42.913 plus 1/2 row v one squared and we get this formula. 00:06:45.217 --> 00:06:49.649 You might think, "Why would we care about this? 00:06:49.649 --> 00:06:53.505 "Who is regularly shooting air at a brick wall?" 00:06:53.505 --> 00:06:55.745 People do it all the time, because you can build 00:06:55.745 --> 00:06:59.536 a pretty important instrument with this called a Pitot tube. 00:06:59.536 --> 00:07:01.849 And the Pitot tube looks something like this. 00:07:01.849 --> 00:07:02.969 Let's get rid of that. 00:07:02.969 --> 00:07:05.193 So why would someone use this system? 00:07:05.193 --> 00:07:07.226 It's called a Pitot tube. 00:07:07.226 --> 00:07:09.360 People use it to measure fluid velocity 00:07:09.360 --> 00:07:11.736 or, if you're moving through the fluid, 00:07:11.736 --> 00:07:14.649 it's a way to measure your velocity or your speed. 00:07:14.649 --> 00:07:16.905 So what happens is you've got this set up. 00:07:16.905 --> 00:07:17.952 Let's say you're in an airplane. 00:07:17.952 --> 00:07:19.176 You mount this on the airplane. 00:07:19.176 --> 00:07:22.128 You're flying through the fluid, which is the air. 00:07:22.128 --> 00:07:26.376 So that mean air is rushing towards this section here. 00:07:26.376 --> 00:07:28.984 Rushing past you, let's say you're flying to the left. 00:07:28.984 --> 00:07:31.752 So you'll notice air flying past you. 00:07:31.752 --> 00:07:34.784 A Pitot tube always has this section that's facing 00:07:34.784 --> 00:07:37.476 into the wind or into the air. 00:07:37.476 --> 00:07:40.413 This air would be directed straight toward this region, 00:07:40.413 --> 00:07:43.714 and the key is this is blocked off at the end. 00:07:43.714 --> 00:07:47.561 So there's air in here, but it can't be moving. 00:07:47.561 --> 00:07:50.185 The air in this section can't be moving all the way 00:07:50.185 --> 00:07:53.257 to the front because, I mean, where's it gonna go? 00:07:53.257 --> 00:07:56.522 We just said if fluid flows it, fluid's gotta flow out. 00:07:56.522 --> 00:07:57.890 There's no out here. 00:07:57.890 --> 00:07:59.266 And then there's another region. 00:07:59.266 --> 00:08:02.586 Up here you've got a second chamber 00:08:02.601 --> 00:08:04.565 where the air flows over the top. 00:08:04.565 --> 00:08:08.229 And this is directed at a right angle to that air flow. 00:08:08.229 --> 00:08:09.172 You've got another chamber. 00:08:09.172 --> 00:08:11.876 And again, in here, fluid's not flowing. 00:08:11.876 --> 00:08:14.896 The key is this gives you a way to determine the difference 00:08:14.896 --> 00:08:17.906 between the pressure here and the pressure there. 00:08:17.906 --> 00:08:20.386 If you had some sort of membrane in here, 00:08:20.386 --> 00:08:24.241 something dividing these two sections that could 00:08:24.241 --> 00:08:26.225 tell you the pressure differential, right? 00:08:26.225 --> 00:08:29.777 If the pressure on this side is a little bigger 00:08:29.777 --> 00:08:33.501 than the pressure on this side, and this would bow outward, 00:08:33.501 --> 00:08:37.009 one of these is measuring the pressure here 00:08:37.009 --> 00:08:40.119 and one of them is measuring the pressure there. 00:08:40.119 --> 00:08:40.724 What is the... 00:08:40.724 --> 00:08:43.323 Mathematically, what's the relationship? 00:08:43.323 --> 00:08:44.595 It's the one we just found. 00:08:44.595 --> 00:08:47.539 Right here, this is the stagnation pressure, right? 00:08:47.539 --> 00:08:49.988 The air's not moving in here, it flowed straight in. 00:08:49.988 --> 00:08:52.227 We know the v is zero right here. 00:08:52.227 --> 00:08:57.227 And so the stagnation pressure equals the pressure up here. 00:08:59.084 --> 00:09:01.588 Again, I'm assuming there's very little height difference. 00:09:01.588 --> 00:09:04.579 Let's say this is a very small device 00:09:04.579 --> 00:09:07.002 and it's not like 10 meters tall. 00:09:07.002 --> 00:09:09.919 So any height differences are minuscule, 00:09:09.919 --> 00:09:11.843 and we would just have our same equation before. 00:09:11.843 --> 00:09:16.843 This would just equal the pressure plus 1/2 row v squared. 00:09:18.995 --> 00:09:20.754 And this is how you determine the velocity 00:09:20.754 --> 00:09:23.826 or the speed, because now we can just solve this for v. 00:09:23.826 --> 00:09:28.826 I'd get that v one equals P s, the stagnation pressure, 00:09:29.143 --> 00:09:32.942 minus the pressure at one, that whole thing, 00:09:32.942 --> 00:09:37.415 times two, divided by the density of the air 00:09:37.415 --> 00:09:38.702 and then a square root because you have to 00:09:38.702 --> 00:09:40.239 solve for the v one. 00:09:40.239 --> 00:09:43.581 So this device lets you determine this 00:09:43.581 --> 00:09:46.332 pressure differential right here, check. 00:09:46.332 --> 00:09:49.076 You need to know what the density of air is 00:09:49.076 --> 00:09:51.079 and this gives you a way to determine the 00:09:51.079 --> 00:09:53.671 velocity of the fluid, or in other words, 00:09:53.671 --> 00:09:57.611 the velocity of your aircraft flying through the air.