![]() |
If this is your first visit, be sure to check out the FAQ by clicking the link above. You may have to register before you can post: click the register link above to proceed. To start viewing messages, select the forum that you want to visit from the selection below. |
|
|
Thread Tools | Display Modes |
#41
|
|||
|
|||
![]() "Ash Wyllie" wrote in message ... Add a touch of quinine to your CO2 + DHMO + ethanol mix, and you have a good anti-malarial compound. Now, what did I do with that mosquito... Hmmmm, first I think you need to compound a small amount of liquidus DHMO and ethanol with the steam distillate of Dipterocarpus cornutus. The result is less volatile and enhances the effect of the quinine. The result, when ingested after having been passed over "en solidus" DHMO will cause impairment of vision in persons with low tolerance. Supporting your claim above, I have not found one case history of malaria involved with this treatment. Hyperingestion, on the other hand, has led to nausea and vomiting, combined with disorentation and cardiovascular depression. |
#42
|
|||
|
|||
![]()
So, lets look at this factually...
In recent history, atmospheric CO2 levels have been at their lowest levels in the entire history of the planet. It has been as low as about 150 ppm. In recent history, it has been steadily climbing toward 300 ppm, presumably due to human activity, but there has been a fair amount of volcanic activity in recent years which also contributes large amounts of CO2. Given the fact that during the age of the dinosaurs, CO2 levels were up around 1,000 to 2,000 ppm, this recent CO2 rise is rather insignificant by comparison. Also, historical global temperature data shows that the earth has a bi-stable average temperature (bouncing between 12C and 22C). The average temperature of the earth is currently at the low bi-stable point, but throughout most of the earths history, the temperature was at the high bistable point. The last time that the earth had the current combination of low CO2 and low average temperature was about 300 million years ago. There is a nice historical summary graph that shows both atmospheric CO2 levels and average temperature that is available at http://www.clearlight.com/~mhieb/WVF...s/image277.gif Dean |
#43
|
|||
|
|||
![]() Dean Wilkinson wrote: So, lets look at this factually... In recent history, atmospheric CO2 levels have been at their lowest levels in the entire history of the planet. You have no way of knowing that. I can just see the caveman out there with his CO2 test kit..... It has been as low as about 150 ppm. In recent history, it has been steadily climbing toward 300 ppm, presumably due to human activity, but there has been a fair amount of volcanic activity in recent years which also contributes large amounts of CO2. It's a guess. We only have maybe 150 years of temp data and much less years of other data. In the history of the planet that is zip. Also, historical global temperature data shows that the earth has a bi-stable average temperature (bouncing between 12C and 22C). The average temperature of the earth is currently at the low bi-stable point, but throughout most of the earths history, the temperature was at the high bistable point. The last time that the earth had the current combination of low CO2 and low average temperature was about 300 million years ago. The earth has cooled and warmed constantly. Glaciers come and go. Humans couldn't change that if they wanted. |
#44
|
|||
|
|||
![]() "Newps" wrote in message ... Dean Wilkinson wrote: So, lets look at this factually... In recent history, atmospheric CO2 levels have been at their lowest levels in the entire history of the planet. You have no way of knowing that. I can just see the caveman out there with his CO2 test kit..... Actually, we do know this with a fair degree of confidence. Antarctica has trapped bubbles of air going way back in its ice that has been core sampled. There are other geologic indicators that they use to determine the levels as well for prehistoric data. It has been as low as about 150 ppm. In recent history, it has been steadily climbing toward 300 ppm, presumably due to human activity, but there has been a fair amount of volcanic activity in recent years which also contributes large amounts of CO2. It's a guess. We only have maybe 150 years of temp data and much less years of other data. In the history of the planet that is zip. There are other geological records that are used to determine temperature besides direct measurements. Also, historical global temperature data shows that the earth has a bi-stable average temperature (bouncing between 12C and 22C). The average temperature of the earth is currently at the low bi-stable point, but throughout most of the earths history, the temperature was at the high bistable point. The last time that the earth had the current combination of low CO2 and low average temperature was about 300 million years ago. The earth has cooled and warmed constantly. Glaciers come and go. Humans couldn't change that if they wanted. |
#45
|
|||
|
|||
![]()
On Mon, 13 Dec 2004 at 03:20:38 in message
, Capt.Doug wrote: No, less air, because the density of the ambient air is less as altitude rises. Less air in the front means less air out the back (though the pressure ratio can be the same). Jet engines produce less thrust at altitude. There is less cooling air which means that maximum exhaust temperature is reached at a lower thrust. The efficiency gains come from the forward speed of the engine (sort of a ram effect) and the lower aerodynamic drag at altitude (higher true airspeed). This interests me as it is often said, the idea of less drag at altitude presumably comes from the idea that drag depends on air density? Which of course it does. However if you fly for maximum range than you fly close to maximum lift/drag ratio which depends only on getting the correct alpha (ignoring compressibility effects). So since lift = weight, drag depends on weight and it reduces as fuel is burned. The aircraft flies faster to create the lift at altitude but the drag is presumably almost the same? Am I wrong? -- David CL Francis |
#46
|
|||
|
|||
![]() Dean Wilkinson wrote: You have no way of knowing that. I can just see the caveman out there with his CO2 test kit..... Actually, we do know this with a fair degree of confidence. Antarctica has trapped bubbles of air going way back in its ice that has been core sampled. Would that be before, during or after the volcanic eruption? While interesting, trapped air doesn't tell us much of anything. We can't even affix a date to within a reasonable amount of time. There are other geological records that are used to determine temperature besides direct measurements. Yes, but today we know what the temp is every hour of every day. Looking at rocks we only have generalities. It was hot during this period of years, cold during this period, etc. Now we're trying to say that because the temp has gone up 1 degree in the last 50 years we have a problem. |
#47
|
|||
|
|||
![]()
"David CL Francis" wrote in message
... [...] So since lift = weight, drag depends on weight and it reduces as fuel is burned. The aircraft flies faster to create the lift at altitude but the drag is presumably almost the same? Am I wrong? Yes. ![]() The drag is actually less. The indicated airspeed is a good way of seeing how the airframe is currently being affected by the ambient air at whatever density it is. Regardless of the air's actual density, the 1G stall speed is always the same, and for constant engine power, cruise speed remains remarkably constant (I'm not sure whether it is actually constant, but having flown a turbocharged engine at altitudes up to 18,000' and noting an airspeed drop only higher than 16,000', the turbocharger's "critical altitude", I am confident in saying that, when measured by indicated airspeed, there's practically no change as long as power is kept constant). As altitude goes up and indicated airspeed remains constant, TRUE airspeed, on the other hand, goes up. Same lift (equal to weight, as you note), but you're going faster for the same power. Obviously thrust didn't increase (and in fact, decreased, since you get less thrust from the prop due to the less dense air...though with a constant speed prop, much if not all of the lost thrust can be regained using coarser prop pitch), so the only way to go faster is for drag to have decreased. Since lift is constant, maximum lift/drag ratio still occurs at the particular angle of attack where drag is minimized. But the ratio is higher, because drag is lower. It's the angle of attack that's constant, not the ratio itself. Pete |
#48
|
|||
|
|||
![]()
Air is pretty heavy, which is why we can fly. It weighs .078
lb/cubic foot at standard sea level pressure and temperature. What's that, about 13 cubic feet for a pound? The air in a room can easily outweigh the occupants. Dan |
#49
|
|||
|
|||
![]() |
#50
|
|||
|
|||
![]()
Air is mostly (70%) Nitrogen, most of the rest is Oxygen.
The atomic mass of Nitrogen is 14, of Oxygen is 16. Both occur as molecules (N2, O2) so the mass of each molecule is twice the above figures. Now, at STP, there are 22.4 liters in a mole, and a mole is the amount of stuff that would weigh (in grams) what its molecular mass is. So, 22.4 liters of nitrogen would weigh 28 grams. Of Oxygen, it would be 32 grams. So we have a little over a gram per liter. Ok, more than just a little, but less than a gram and a half per, and it's in the ballpark. Lets use one gram per liter. A liter is 1000 cubic centimeters, which is the volume of a cube 10 centimeters on a side. (or equivealently, 1/10 meter on a side). 1000 liters would be a cube one meter on a side, and air would weigh "a little" over one Kg per cubic meter. A meter is "a little" over three feet, so a cubic meter is "a little more" over 27 cubic feet. One Kg is "a little" over two pounds, divide by 27, or even 30, and I get something less than a tenth of a pound per cubic foot. Air is pretty heavy, which is why we can fly. It weighs .078 lb/cubic foot at standard sea level pressure and temperature. What's that, about 13 cubic feet for a pound? Yep. That's just about right. Now, take a typical room that's three meters tall, three meters wide, and four meters deep. Not a very big room, but it has a high ceiling. This gives us 36 cubic meters, and the air would weigh "a little" over 36 Kg. Well, I weigh more than a little over 36 Kg, but it's close enough to show that a smallish room will hold less than a person's mass in air, but a largish roomfull of air can easily outweigh a person. The air in a room can easily outweigh the occupants. Yep again. Now, how big is the White House? Jose -- Freedom. It seemed like a good idea at the time. for Email, make the obvious change in the address. |
Thread Tools | |
Display Modes | |
|
|