Calcs
Made a few excel calcs for compression ratio, supercharger max impeller speed and static compression ratio.
once again needs a place to live ftp/website this is an image of the excel file.
Feel free to add in your imput. (and check my math...)
once again needs a place to live ftp/website this is an image of the excel file.
Feel free to add in your imput. (and check my math...)
Hey...can you input a multiplier that compensates for altitude for us high elevation guys? I believe we can run a bit more boost because effective pressure is a good bit lower up here. (5500 ft ASL)
ABV, the formula is:
Effective CR = (Boost + ATM_PSI) * CR / ATM_PSI
The problem is that I don't know what the multiplier is for every 500 ft of altitude (or 1000 or whatever). Here's a chart of what happens:
http://www.engineeringtoolbox.com/air-alti...sure-d_462.html
If we look at pressure at sea level relative to every 500 ft of altitude, it appears that for every 500 ft of altitude pressure drops at a mildly exponential rate. At first the drop is .27 psi for the first 1000 ft or so, then .26, then .25...
I don't know how I would make a multiplier for something that is non-linear. There aren't that many of them. Maybe you could do something like, if x > 0 and x < 500, use .27. if x > 500 and x < 1000, use .27...
Something like that since there aren't many of them? I found a calculator online a long time ago and it was awesome. I found at that at 5000 ft, the effective compression ratio of our motors sanz FI is like 10:1 or something like that.
Ah! Just found it. Check this:
http://www.rbracing-rsr.com/compression.htm
Can someone view the source on that and translate the code?
Effective CR = (Boost + ATM_PSI) * CR / ATM_PSI
The problem is that I don't know what the multiplier is for every 500 ft of altitude (or 1000 or whatever). Here's a chart of what happens:
http://www.engineeringtoolbox.com/air-alti...sure-d_462.html
If we look at pressure at sea level relative to every 500 ft of altitude, it appears that for every 500 ft of altitude pressure drops at a mildly exponential rate. At first the drop is .27 psi for the first 1000 ft or so, then .26, then .25...
I don't know how I would make a multiplier for something that is non-linear. There aren't that many of them. Maybe you could do something like, if x > 0 and x < 500, use .27. if x > 500 and x < 1000, use .27...
Something like that since there aren't many of them? I found a calculator online a long time ago and it was awesome. I found at that at 5000 ft, the effective compression ratio of our motors sanz FI is like 10:1 or something like that.
Ah! Just found it. Check this:
http://www.rbracing-rsr.com/compression.htm
Can someone view the source on that and translate the code?
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kamehamaha
S2000 Under The Hood
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Dec 5, 2001 08:51 AM



