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On Feb 5, 7:00 am, Mxsmanic wrote:
Stubby writes: First, lift is proportional to mass-air flow over a curved surface. A curved surface has nothing to do with lift. Riiiight. NACA sections are just to make the wing look pretty |
#2
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george writes:
Riiiight. NACA sections are just to make the wing look pretty No, they reduce drag and increase the range of angles of attack through which lift is produced. The curves are not necessary for lift. -- Transpose mxsmanic and gmail to reach me by e-mail. |
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john smith wrote:
Here is a question to challenge your understanding of engine operation... During Winter in the colder climes, do you use less fuel when you fly because the air is more dense? It takes less energy to compress air in the cylinder (or in any other centrifugal or axial compressor) at lower temperature so I would say that the thermodynamic cycle (in a reciprocating engine or gas turbine) is more efficient. |
#4
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The higher the density altitude, you get better gas mileage for a give
TAS. So colder means lower density altitude and WORSE gas mileage (everything else being equal, which it probably isn't). There may be some other things going on, I am not sure about them. You will be able to climb better and go faster at full throttle when it is cold. |
#5
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![]() "Doug" wrote in message ups.com... The higher the density altitude, you get better gas mileage for a give TAS. So colder means lower density altitude and WORSE gas mileage (everything else being equal, which it probably isn't). There may be some other things going on, I am not sure about them. You will be able to climb better and go faster at full throttle when it is cold. This last part is more correct/to the point. In colder weather, your engine CAN develop more power. Power = Fuel. In cold weather you can go FASTER because your engine can develop more POWER. For a given engine, faster means less MPG. |
#6
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![]() "Matt Barrow" wrote in message ... "Doug" wrote in message ups.com... The higher the density altitude, you get better gas mileage for a give TAS. So colder means lower density altitude and WORSE gas mileage (everything else being equal, which it probably isn't). There may be some other things going on, I am not sure about them. You will be able to climb better and go faster at full throttle when it is cold. This last part is more correct/to the point. In colder weather, your engine CAN develop more power. Power = Fuel. In cold weather you can go FASTER because your engine can develop more POWER. For a given engine, faster means less MPG. Let's beat this dog some more. Going faster also means less time required to get to the destination. Considering that as pilots we are more interested in fuel consumption, gallons per hour, than MPG is it more economical to fly faster/higher? Let's presume a 250NM trip at 10Kft [for the nitpickers, the wind is nil both ways]. According to the POH for the C-172M that I fly the trip will take 2.8 hours and burn 15.4 gallons at 89 KTAS. Shove the throttle to the firewall and the trip will take 2.1 hours and burn 15.9 gallons at 119 KTAS. To steal a line from Paul Harvey; "And now, the rest of the story." At first glance, it is going to cost more to fly faster. But the analysis isn't quite over, yet. Let's pay $4/Gal for the fuel, that means I paid $2 more for fuel to go the distance. But the airplane is also costing me an hourly rate of about $85. By flying faster, I shaved off 0.7 hours. or $59.5. We could extend this into other cost advantages, such as extending the miles flown between overhauls, but I think I've made my point. My point is, you may get more miles per gallon at the penalty of other expenses. When you are cruising, push the throttle to the firewall and screw the friction lock down -- but by all means keep the engine properly leaned. |
#7
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On Mon, 05 Feb 2007 17:30:43 GMT, "Casey Wilson"
wrote: "Matt Barrow" wrote in message ... "Doug" wrote in message ups.com... The higher the density altitude, you get better gas mileage for a give TAS. So colder means lower density altitude and WORSE gas mileage (everything else being equal, which it probably isn't). There may be some other things going on, I am not sure about them. You will be able to climb better and go faster at full throttle when it is cold. This last part is more correct/to the point. In colder weather, your engine CAN develop more power. Power = Fuel. In cold weather you can go FASTER because your engine can develop more POWER. For a given engine, faster means less MPG. Let's beat this dog some more. Going faster also means less time required to get to the destination. Considering that as pilots we are more interested in fuel consumption, gallons per hour, than MPG is it more economical to fly faster/higher? Let's presume a 250NM trip at 10Kft [for the nitpickers, the wind is nil both ways]. According to the POH for the C-172M that I fly the trip will take 2.8 hours and burn 15.4 gallons at 89 KTAS. Shove the throttle to the but at 10,000 feet you probably will not be able to get more than 55 to 60% power full throttle in a normally aspirated engine. In the Deb I find maximum true speed comes some where between 6000 and 8000 feet depending on temperature. firewall and the trip will take 2.1 hours and burn 15.9 gallons at 119 KTAS. almost 16 in a 172 just doesn't sound right even at maximum crusise at lower altitudes let alone 10,000 I only burn 14 at 75% in the Deb witha 260 HP, 6-cylinder IO-470N engine. At 10,000 the fule burn is down to about 12.5. To steal a line from Paul Harvey; "And now, the rest of the story." At first glance, it is going to cost more to fly faster. But the analysis isn't quite over, yet. Let's pay $4/Gal for the fuel, that means I paid $2 more for fuel to go the distance. But the airplane is also costing me an hourly rate of about $85. By flying faster, I shaved off 0.7 hours. or $59.5. We could extend this into other cost advantages, such as extending the miles flown between overhauls, but I think I've made my point. My point is, you may get more miles per gallon at the penalty of other expenses. When you are cruising, push the throttle to the firewall and screw the friction lock down -- but by all means keep the engine properly leaned. Roger Halstead (K8RI & ARRL life member) (N833R, S# CD-2 Worlds oldest Debonair) www.rogerhalstead.com |
#8
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Let's say you keep your TAS the same. Now, up high, you can't go as
fast as down low, full throttle. But at full throtte at 10,000' DENSITY ALTITUDE say you have a TAS of 120 knots, and a manifold pressure of 20". You burn, 8 gph, getting 15 miles/gallon. Now at 5000' DENSITY ALTITUDE, to run at the same 120 Knots TAS, you need 22" of manifold pressure, and burn 9 gph, getting 13.3 miles/ gallon. Now, when it gets colder, the same true altitude is a lower density altitude. So running at the same TAS, when it is cold, you get worse fuel mileage than when it is warm. So if you keep the TAS the same, the true altitude the same, the barometric pressure the same, you will get WORSE gas mileage when it gets colder. |
#9
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![]() "Roger" wrote in message ... On Mon, 05 Feb 2007 17:30:43 GMT, "Casey Wilson" wrote: firewall and the trip will take 2.1 hours and burn 15.9 gallons at 119 KTAS. almost 16 in a 172 just doesn't sound right even at maximum crusise at lower altitudes let alone 10,000 I only burn 14 at 75% in the Deb witha 260 HP, 6-cylinder IO-470N engine. At 10,000 the fule burn is down to about 12.5. Roger Halstead (K8RI & ARRL life member) (N833R, S# CD-2 Worlds oldest Debonair) www.rogerhalstead.com Hi Roger, That was 15.9 gallons start to finish, not GPH ![]() Casey |
#10
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![]() "Casey Wilson" wrote in message news:7RJxh.1999$5U4.453@trnddc07... "Matt Barrow" wrote in message In colder weather, your engine CAN develop more power. Power = Fuel. In cold weather you can go FASTER because your engine can develop more POWER. For a given engine, faster means less MPG. Let's beat this dog some more. Going faster also means less time required to get to the destination. Considering that as pilots we are more interested in fuel consumption, gallons per hour, than MPG is it more economical to fly faster/higher? Let's presume a 250NM trip at 10Kft [for the nitpickers, the wind is nil both ways]. According to the POH for the C-172M that I fly the trip will take 2.8 hours and burn 15.4 gallons at 89 KTAS. Shove the throttle to the firewall and the trip will take 2.1 hours and burn 15.9 gallons at 119 KTAS. Your TAS increases 33%, but your Fuel Flow increases only 4%? My fuel flow doubles between Econ Cruise and Max Cruise (9.4 gph/172kts vs 18.4gph/205kts). Check your data. |
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