I'm not sure I completely understand. Air pressure decreases directly corresponding to feet above sea level, and besides that, humidity and high temperature dilute and reduce the amount of air per volume. But do you think 80F is a more realistic input for temperature in Denver than 60F? Even if not I guess your value might stand if it were made up for by humidity being above 0- I don't know how the sensitivity to change in humidity compares to the sensitivity to temperature.Rich Euro M5 wrote:It's even worse for the NA cars because of density altitude. Density altitude can be loosely thought of as the apparent altitude (what the engine thinks it's operating at) vs true altitude referenced to Mean Sea Level "MSL". Density altitude is what aviators use to understand aircraft performance during nonstandard conditions. Standard altitude in the US is based on a standard of 29.92" HG and 68 F. air temp at 0% humidity. For aviation / performance calculations density altitude calculations are based a two measurable values, pressure altitude (1 BAR ~15 psi reference) and air temperature. Since I happen to have my handy E6B whizwheel I ran a quick exercise to see how non-standard temps impact DA when pressure is constant. If the airtemp increases from 15C (~60F) to 27 C (~80F) you'll see a DA of about 3000 ft. So in Houston which is about 50 ' MSL at 80F the engine thinks it's at ~ 3000 ft.T_C_D wrote:TurboDan is racing n/a cars at elevation of 5500 feet so he has a huge advantage with his turbo car.
Extrapolate this DA increase to Denver and you quickly can see that a NA car's engine is seeing a DA of ~ 8500' not 5500 '. In aviation circles there's a rule of thumb that 75% power will be seen at about 7500 ' of altitude during standard conditions. So you can see that at Denver altitudes during a standard day you'll only make about 80% of the theoretical HP. If the outside air temp are above standard conditions the performance will suffer even further.
Depending on how well Dan's turbo car is running he might have HP values comparable to some pretty high HP NA cars.
Rich
But don't these factors apply to Dan as well? It seems like everybody else is clear on this, but I'm not... isn't his boost just above ambient air pressure? I'm not sure why the thin air is assumed to affect only NA cars and is an advantage for a turbo.
Also, I think you went the wrong direction estimating the power percentage remaining at elevation. If you've got 75% at 7500, you would expect the effect to be more pronounced as effective elevation continues to increase, so DA = 8500, power would be even lower, maybe 70%. But then you went on to say that if air temps were higher the effect would be even more, so maybe the 80% is humidity adjusted? I'm not sure what you were doing there.
Not to pick you apart, you made an interesting point there. I'm just curious. I've been working with gravity anomalies some, which are similar. Also, I'm about to fly to 5000 feet, and I hope to get up to near twice that, so it'd be nice to know exactly why I'm feeling so shitty!