TonyWilliams
Well-known member
- Joined
- Apr 14, 2013
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- 572
nozferatu said:To compare, drag area is the frontal area times drag coefficient. The Prius has a drag area of 6.2 sq ft. The Spark EV has a drag area of 8.8 sq ft. That's almost 30% more.
Referring to my previous equations, one thing to remember is that density over temperature doesn't play much of a role at a specific altitude. For three reasons...1) the variation in density with temperature is about 0.002 kg/m^2 per degree F for a set altitude..say at sea level or 500ft or whatever one would expect a car to be at in everyday normal driving.
Well, folks "normally" drive at all elevations and all temperatures. Just because your "normal" is at sea level with southern California non-weather does NOT mean that both temperature AND elevation are not important to the equation of air density.
Here's some examples of "air density equivalent elevation" in feet above seal level and the relative density to "standard" (standard is sea level, 59F, air pressure 29.92 inches), which will mean a whole lot more to folks than "0.002 kg/m^2 per degree F". I have omitted the variations in standard pressure, since those are indeed smaller adjustments (that you make no mention of). Humidity is also omitted, even though it also has a small impact on air density:
Temperature ------ Sea level -------- 5000 feet --------- 10000 feet
-------------------Santa Barbara------- Denver -------- mountain pass
-40F -------minus 8000 ft (123%) - minus 900 ft (102%)--- +5500 ft (85%)
59F ---------- sea level (100%) ----- +6200 ft (83%) ------ +12200 ft (69%)
120F ----------- +3800 (90%) ------ +9800 ft (74%) ------ eh, not really possible!
The point of this exercise is to show that temperature is a LARGE determiner of air density. Through the temperature extremes that one might find on inhabited portions of planet earth, air density can change more than 30% at the same elevation.
You'll also be advised that your metric air pressure density is kg/m^3, not ^2, as you write:
Temp -------sea level ----------- 5000 feet ---------- 10000 feet
-40F ----- 1.513kg/m^3 ------ 1.259kg/m^3 ------ 1.04kg/m^3
59F ------ 1.224kg/m^3 ------ 1.019kg/m^3 ------ 0.842kg/m^3
120F ----- 1.095kg/m^3 ----- 0.911kg/m^3 ------- 0.753kg/m^3
Air density at the same elevation is 1/3 less at the same temperature, from sea level to 10,000 feet elevation.
It is also 1/3 less at the same altitude, between -40F and +120F.
2) it's a linear relation within the equation unlike velocity that increases on a squared relationship.
So, because the variable is linear, you omit it? There are other linear data points, too.