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How DA affects Compression?

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Old Jul 8, 2006 | 07:07 PM
  #21  
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Originally Posted by Old SStroker
As you increase altitude your Indicated Airspeed drops, but your True Airspeed stays the same or increases. Indicated Airspeed can be thought of as the number of molecules you plow thru in a period of time, while True Airspeed is how fast you pass each molecule.

A jet transport that cruises at 650 mph (true A/S) at altitude would have trouble going that fast near sea level.
Hence the 18,000 mph speeds achieved in space...
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Old Jul 8, 2006 | 07:10 PM
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Originally Posted by BlackHawk T/A
Actually Houston is under 2000, even being as insanely humid as it is right now, if the numbers are correct. Looks like elevation plays a much bigger role than humidity. In comparison i'm sitting at about 3000 DA.
Humidity has a small effect on DA, actual altitude and temperature has a huge effect. Ive seen as low as -2000 at Houston Raceway Park and it makes several mph difference in trap speed on my car, from a +2000 day.
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Old Jul 8, 2006 | 07:35 PM
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Originally Posted by AOC
Wow, 8,000 DA??? And I thought we had it bad when we reach 3000 DA. lol.

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
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Old Jul 8, 2006 | 09:10 PM
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Still quite an achievement up here Frank, and it looked damn good doing it too.

J
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Old Jul 8, 2006 | 09:22 PM
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From what I understand, I actually lose about .5 points of compression living here in the Denver area. Less air to compress.

Makes that 12.64/115 look decent.
Stock gears, stock rear, crap launch, etc.
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Old Jul 8, 2006 | 09:43 PM
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Originally Posted by sscam68
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

yeah, guys crying for 12s at real low DAs crack me
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Old Jul 8, 2006 | 10:30 PM
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When building an engine for high altitude you can really up the compression. If the air is 20% less dense, you can up the compression by 20%.
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.
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Old Jul 8, 2006 | 11:29 PM
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Originally Posted by CamKing
When building an engine for high altitude you can really up the compression. If the air is 20% less dense, you can up the compression by 20%.
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.
Thank you!

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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Old Jul 9, 2006 | 08:27 AM
  #29  
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Originally Posted by cantdrv65
Hence the 18,000 mph speeds achieved in space...

DA @ 200 miles up must be hard to figure, huh?

So why are they going ~18,000 mph? Why not ~24,000?
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Old Jul 10, 2006 | 11:24 AM
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Originally Posted by Old SStroker
DA @ 200 miles up must be hard to figure, huh?

So why are they going ~18,000 mph? Why not ~24,000?
If we had a space-based refueling station they would go faster than that.
Breaking free of the Earth uses up almost all of the fuel.
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Old Jul 10, 2006 | 11:54 AM
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Originally Posted by white2001s10
If we had a space-based refueling station they would go faster than that.
Breaking free of the Earth uses up almost all of the fuel.
Let me rephrase the question:

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?
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Old Jul 10, 2006 | 01:33 PM
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think of it this way. at sea level you have 14.7psi of natural boost. the higher up you go the less natural boost you have hence less power.
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Old Jul 10, 2006 | 03:02 PM
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The DA in Flagstaff the other day was 12,000+ lol
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Old Jul 10, 2006 | 08:05 PM
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Originally Posted by sscam68
I'm thinking about a cam but would like something designed for our particular application. Got any recommendations?
I'm sure I can figure it out.
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.
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Old Jul 10, 2006 | 08:07 PM
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Originally Posted by Wnts2Go10O
think of it this way. at sea level you have 14.7psi of natural boost. the higher up you go the less natural boost you have hence less power.
I think that's a great way to explain it.
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.
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Old Jul 10, 2006 | 09:08 PM
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Originally Posted by Speed Density
Just wondering why in higher DAs you have to run less compression, wereas in lower DA you can run much more.
****, just add some boost to it already - I still have a LT1 kit and could make a few more pretty easy
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Old Jul 10, 2006 | 10:01 PM
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Originally Posted by CamKing
I'm sure I can figure it out.
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.
If it works out better for the designer I will not hesitate to remove the top end and ship it out so that an optimal grind can be cut.

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
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Old Jul 11, 2006 | 08:40 AM
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Originally Posted by sscam68
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 at 6,000-9,000 feet.
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.

Not to go to far off on a tangent, would the port design, both intake and exhaust, differ greatly for a high altitude app?
Yes, you would end up with a head that is pretty close to a restrictor plate head. I normally like to see an Exhaust/intake flow ratio of about 74-76% in the mid-lifts(.300"-.500"). For high altitude, you could drop that down to 64-68%.
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Old Jul 11, 2006 | 09:45 AM
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There is compelling logic to the argument that valve events need to be altered to best utilize the reduced air pressure at higher altitudes, but... Several books I have read on turbocharging say that for a well-matched system (in which exhaust back pressure is about the same as boost, unlike a typical bolt-on where the ratio can be as high as 2:1) there is essentially no change required to valve timings.
If no change is required for say plus 20 psi, then surely the same holds true for minus 3 or 4?
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Old Jul 11, 2006 | 11:02 AM
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Originally Posted by MadBill
Several books I have read on turbocharging say that for a well-matched system (in which exhaust back pressure is about the same as boost, unlike a typical bolt-on where the ratio can be as high as 2:1) there is essentially no change required to valve timings.
Those books are flat-out wrong. A turbo engine doesn't require as much valve lift or exhaust duration as a NA engine. It also doesn't require as big of an intake port. A turbo engine also reqires a different exhaust profile then a Blower engine running the same amount of boost. I've been designing cams for Turbo race engines for over 20 years, Including the Buick Indy V6 project and Cosworth Indy cams for many teams including Penske. My father was a well know expert in Turbocharging and consulted for many of the F1 teams when they first went to Turbos. He's also written a few SAE papers on Tubocharging.
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