How DA affects Compression?
A jet transport that cruises at 650 mph (true A/S) at altitude would have trouble going that fast near sea level.
pfft, I wish would could get that.
We've had a fluke of cold weather here in Albuqueruqe. I about shat my pants when I found out the DA was 7400ft. Usually around this time of year its 9000ft.
Was able to run a 12.51@107.9 on a 1.68 60'. Full bolt on 3100lb car with 4.30 gears.
easily an 11 second car at sea level
Makes that 12.64/115 look decent.

Stock gears, stock rear, crap launch, etc.
We've had a fluke of cold weather here in Albuqueruqe. I about shat my pants when I found out the DA was 7400ft. Usually around this time of year its 9000ft.
Was able to run a 12.51@107.9 on a 1.68 60'. Full bolt on 3100lb car with 4.30 gears.
easily an 11 second car at sea level

yeah, guys crying for 12s at real low DAs crack me
You can also cut your exhaust duration down because you are puting 20% less air(lbs/hr) into the engine. You treat the engine a lot like you do a restrictor plate engine.
The only thing you need to change is to put a bigger radiator on the car, because there is less air to cool it.
You can also cut your exhaust duration down because you are puting 20% less air(lbs/hr) into the engine. You treat the engine a lot like you do a restrictor plate engine.
The only thing you need to change is to put a bigger radiator on the car, because there is less air to cool it.
I was wondering how a cam grinder would look at our situation. Given our altitude a lot of the "off the shelf" grinds I don't think would work really well up here.
I'm thinking about a cam but would like something designed for our particular application. Got any recommendations?
Last edited by sscam68; Jul 8, 2006 at 11:46 PM.
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So why are they going ~18,000 mph? Why not ~24,000?
Breaking free of the Earth uses up almost all of the fuel.
Breaking free of the Earth uses up almost all of the fuel.
What happens below about 18,000 mph to a craft launched from Earth?
What happens above about 24,000 mph to a craft launched from Earth?

PM me with all your specs and I'll get you a recommendation.
I've made a bunch of racing cams for high altitude, I'll just need to know if your planning on running it at lower altitudes also.
Normal N.A. cams and engines are designed for 14.697psi of boost, and if you don't have that much boost you need to change the design.
PM me with all your specs and I'll get you a recommendation.
I've made a bunch of racing cams for high altitude, I'll just need to know if your planning on running it at lower altitudes also.
In my particular app. the DA ranges from 9000ft in the summer (worst case scenario) to 6000ft in the winter.
In general, how would the cam design differ? What would be the design considerations? Mind you this is more of strip app. than a street. What kind of a static compression would work better? A lot of people with AFR combos are having the heads milled and ending up with a static compression of 11:1
(roughly). According to what you posted, if I were to up the compression 20% I would end up with a 13.2:1 static compression
. Maybe it's just me, but isn't that just a tad too high?Not to go to far off on a tangent, would the port design, both intake and exhaust, differ greatly for a high altitude app?
Frank
. Maybe it's just me, but isn't that just a tad too high?Some of the differences in cam design would be more area on the intake and less on the exhaust.
For me to figure out what you need, I need the Bore, Stroke, Rod Length, Peak HP RPM desired, RPM you want to launch at, Injector throttle body size, Comp ratio, Port Flow #'s, and Rocker Ratio.
If no change is required for say plus 20 psi, then surely the same holds true for minus 3 or 4?

