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The Mooney 201 has a ram air port, a half a foot under the prop
spinner. The POH tells us it can be opened at altitude for a very modest increase in MP and we find maybe a half inch increase in pressure. The idea of the thing is, if the port is looking right at the air being thrust toward it by the prop (it can't be more than 6 inches or so behind it) as well as the air impact from the airplane's motion the air being 'rammed' into it should effectively lower the altitude the engine thinks it's at. Well, a half inch of Hg is about 500 feet or so. The question is, though, wouldn't you think there would be a way to capture a great deal more of the ram air effect and really boost the engine performance? Who wouldn't like to fly at 24 square at 12000 feet without a turbo charger? What makes me wonder about it is, even at 60 mph holding your hand out of the window of a car subjects it to a significant backward pressure, so the energy must be there. |
#2
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On Jun 1, 8:35*pm, Tina wrote:
The Mooney 201 has a ram air port, a half a foot under the prop spinner. The POH tells us it can be opened at altitude for a very modest increase in MP and we find maybe a half inch increase in pressure. The idea of the thing is, if the port is looking right at the air being thrust toward it by the prop (it can't be more than 6 inches or so behind it) *as well as the air impact from the airplane's motion the air being 'rammed' into it should effectively lower the altitude the engine thinks it's at. Well, a half inch of Hg is about 500 feet or so. The question is, though, wouldn't you think there would be a way to capture a great deal more of the ram air effect and really boost the engine performance? Who wouldn't like to fly at 24 square at 12000 feet without a turbo charger? What makes me wonder about it is, even at 60 mph holding your hand out of the window of a car subjects it to a significant backward pressure, so the energy must be there. An interesting question. I will have a stab at it but its just an intuitive guess. Thrust is created by the prop pushing the air backwards. If you are trying to capture that air into the engine, there must be some resistance and therefore if you restrict the ability of the air to be pushed away the thrust would be reduced. So it must be a balance between not reducing the thrust and getting more air into the engine to generate more power. I am also guessing that for the ram air to be of much use it would probably be bypassing the airfilter, which is potentially not good for the engine. although at high altitude it is probably Ok, except perhaps for ice formation if there was a lot of moisture in the air? Isnt a Mooney fast enough for you Tina? Terry |
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#4
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The m20J is pretty slippery already and when it was introduced in the
70s was a big step up in efficiency in a production airplane. Homebuilts do do an even better job of cleaning up aerodynamically. The little seals on the flaps and so on were lipstick, the real gain over the Mooney Executive had to do with the 201 getting a more aerodynamic windscreen and engine cowling. We have no serious complaints at all about the airplane (well, in a rainstorm getting in without getting the seat wet is difficult, checking the fuel is hard on pantyhose sometimes) but finding a couple more inches of manifold pressure would be very handy when trying to get to 12000 feet quickly. Once there, we can sip 8 gallons an hour and move along pretty well. I think using ram air would not increase aerodynamic drag, B. Instead of having the air moving at the airplane's airspeed plus prop induced speed impacting the cowling, it could in fact be going into a hole. It's only a 360 cubic inch engine turning at 2300 RPM or so. Isn't that a demand of, let's see, at 23 inches mp at sea level that's 23/30 * 2300/2 * 360 / 12^3 or 180 cubic feet a minute? I better leave that to the engineers. On Jun 1, 7:57 am, Bertie the Bunyip wrote: Tina wrote in news:f9933f5e-0c1d-464b-a1d8- : The Mooney 201 has a ram air port, a half a foot under the prop spinner. The POH tells us it can be opened at altitude for a very modest increase in MP and we find maybe a half inch increase in pressure. The idea of the thing is, if the port is looking right at the air being thrust toward it by the prop (it can't be more than 6 inches or so behind it) as well as the air impact from the airplane's motion the air being 'rammed' into it should effectively lower the altitude the engine thinks it's at. Well, a half inch of Hg is about 500 feet or so. The question is, though, wouldn't you think there would be a way to capture a great deal more of the ram air effect and really boost the engine performance? Who wouldn't like to fly at 24 square at 12000 feet without a turbo charger? What makes me wonder about it is, even at 60 mph holding your hand out of the window of a car subjects it to a significant backward pressure, so the energy must be there. Didn't know any production aircraft had that. Well, to some extent almost every lightplane does . that's why the carb air intake faces forwards in most of them.Everything is a balancing act with an airplane. More air = more drag. You could try putting a couple of woks with tubes out the back to boost your MP, but you're going to pay for it. !Moooney must have spotted an area of the cowl that would not penalise you in this way and decided to utilise it. Really clever homebuilders do a lot of this kind of stuff as well as, and probably more more importantly, dealing with cooling drag. Have you put the other speed mods on your airplane? I think there's nearly ten knots available in seals and various other tidy it up fairings. Bertie |
#5
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![]() "Tina" wrote in message ... The m20J is pretty slippery already and when it was introduced in the 70s was a big step up in efficiency in a production airplane. Homebuilts do do an even better job of cleaning up aerodynamically. The little seals on the flaps and so on were lipstick, the real gain over the Mooney Executive had to do with the 201 getting a more aerodynamic windscreen and engine cowling. We have no serious complaints at all about the airplane (well, in a rainstorm getting in without getting the seat wet is difficult, checking the fuel is hard on pantyhose sometimes) but finding a couple more inches of manifold pressure would be very handy when trying to get to 12000 feet quickly. Once there, we can sip 8 gallons an hour and move along pretty well. I think using ram air would not increase aerodynamic drag, B. Instead of having the air moving at the airplane's airspeed plus prop induced speed impacting the cowling, it could in fact be going into a hole. It's only a 360 cubic inch engine turning at 2300 RPM or so. Isn't that a demand of, let's see, at 23 inches mp at sea level that's 23/30 * 2300/2 * 360 / 12^3 or 180 cubic feet a minute? I better leave that to the engineers. Yes, you are sucking it up as you are trying to push it in, the air that is, and the free airstream is not a very good 'pump'. A turbo with its sealed compressor is much better because once the air is captured it really has a hard time flowing out backwards. |
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#7
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On Jun 1, 6:21*am, Tina wrote:
The m20J is pretty slippery already and when it was introduced in the 70s was a big step up in efficiency in a production airplane. Homebuilts do do an even better job of cleaning up aerodynamically. The little seals on the flaps and so on were lipstick, the real gain over the Mooney Executive had to do with the 201 getting a more aerodynamic windscreen and engine cowling. We have no serious complaints at all about the airplane (well, in a rainstorm getting in without getting the seat wet is difficult, checking the fuel is hard on pantyhose sometimes) but finding a couple more inches of manifold pressure would be very handy when trying to get to 12000 feet quickly. Once there, we can sip 8 gallons an hour and move along pretty well. You don't get a couple inches on the 201. You will hardly notice the difference and most 201 owners remove the cabling since it adds complexity to annual (having to drop the cowl and re-rig the cable each time). In the pre-201's it adds 3/4 of an inch. The 201 easily gets to 12,000 feet. I live at the foot of the Sierras and sometimes cross at 16,000 without turbo. If you don't have it already most of us consider an engine monitor to be minimum equipment for take off. Add to that a fuel computer (I wouldn't own a plane without one) and you can really manage your fuel. -Robert, Mooney CFII |
#8
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![]() "Bertie the Bunyip" wrote in message ... Didn't know any production aircraft had that. Well, to some extent almost every lightplane does . that's why the carb air intake faces forwards in most of them.Everything is a balancing act with an airplane. More air = more drag. You could try putting a couple of woks with tubes out the back to boost your MP, but you're going to pay for it. !Moooney must have spotted an area of the cowl that would not penalise you in this way and decided to utilise it. Really clever homebuilders do a lot of this kind of stuff as well as, and probably more more importantly, dealing with cooling drag. Have you put the other speed mods on your airplane? I think there's nearly ten knots available in seals and various other tidy it up fairings. Bertie Dumb ass. Its because the size of the scoop increases volume (not pressure), and you already have too much. |
#9
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"Maxwell" luv2^fly99@cox.^net wrote in
: "Bertie the Bunyip" wrote in message ... Didn't know any production aircraft had that. Well, to some extent almost every lightplane does . that's why the carb air intake faces forwards in most of them.Everything is a balancing act with an airplane. More air = more drag. You could try putting a couple of woks with tubes out the back to boost your MP, but you're going to pay for it. !Moooney must have spotted an area of the cowl that would not penalise you in this way and decided to utilise it. Really clever homebuilders do a lot of this kind of stuff as well as, and probably more more importantly, dealing with cooling drag. Have you put the other speed mods on your airplane? I think there's nearly ten knots available in seals and various other tidy it up fairings. Bertie Dumb ass. Its because the size of the scoop increases volume (not pressure), and you already have too much. Nope. Bertie |
#10
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![]() "Bertie the Bunyip" wrote in message ... "Maxwell" luv2^fly99@cox.^net wrote in : "Bertie the Bunyip" wrote in message ... Didn't know any production aircraft had that. Well, to some extent almost every lightplane does . that's why the carb air intake faces forwards in most of them.Everything is a balancing act with an airplane. More air = more drag. You could try putting a couple of woks with tubes out the back to boost your MP, but you're going to pay for it. !Moooney must have spotted an area of the cowl that would not penalise you in this way and decided to utilise it. Really clever homebuilders do a lot of this kind of stuff as well as, and probably more more importantly, dealing with cooling drag. Have you put the other speed mods on your airplane? I think there's nearly ten knots available in seals and various other tidy it up fairings. Bertie Dumb ass. Its because the size of the scoop increases volume (not pressure), and you already have too much. Nope. Bertie How would you know, dumb ass? |
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