I got a good question for you cam guys
with both cams go ahead and assume the LSA, ground in advance and other variables are the same (unless you think that would come into play)
Im not sure that there is a diff but with the smaller cam and 1.8 rockers you would have less velocity (or range of movement) on the lifters and pushrod but more pressure (i think)
And then with the bigger cam and 1.7 rockers you would have more velocity velocity (or range of movement) but less pressure on them ( i think)
Please feel free to elaborate as much as you feel like on this idea and your opinion on it, or just tell me im an idiot and it doest make a differece. Or if i stumped you, let me know so i feel good about myself.
To answer the question simply though ,total lift will be roughly same.
Last edited by Joe Overton; Oct 22, 2005 at 09:29 AM.
Thanks
Rob
Thanks
Rob
Thanks
Rob
But like I said, I could be wrong, as I'm certainly no expert.

Josh
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But like I said, I could be wrong, as I'm certainly no expert.

Josh
The Best V8 Stories One Small Block at Time
Thanks for the correction, now that I think about it you are definately correct. I was looking at it without taking into account a number of other factors. In the example Josh gave, of the cam with a V vs. the cam with the U lobes, what would these different characteristics be considered? Are these the ramp rates? and would the cam w/ the U lobe be considered to have more overall duration or would they both have the same duration?
I would think they would have the same duration at .05" lift but very different characteristics once the valves started opening more.
Thanks for the correction. I'm relatively new to this stuff and trying very hard to learn so bear with me please =).
I love this new forum, I learn new stuff everyday here.
Rob
Last edited by Robs98SS; Oct 22, 2005 at 01:27 PM.
Thanks for the correction, now that I think about it you are definately correct. I was looking at it without taking into account a number of other factors. In the example Josh gave, of the cam with a V vs. the cam with the U lobes, what would these different characteristics be considered? Are these the ramp rates? and would the cam w/ the U lobe be considered to have more overall duration or would they both have the same duration?
I would think they would have the same duration at .05" lift but very different characteristics once the valves started opening more.
Thanks for the correction. I'm relatively new to this stuff and trying very hard to learn so bear with me please =).
I love this new forum, I learn new stuff everyday here.
Rob
https://ls1tech.com/forums/advanced-engineering-tech/396086-camshaft-discussion-part-ii.html
https://ls1tech.com/forums/advanced-engineering-tech/394934-camshaft-discussion-part-iii.html
All though there is a lot of text, It will go over a lot of details such as cam lobe shape. A quick brief explanation:
Lobe A) Comp Lobe # 3728
285* duration @ .006
236* duration @ .050
157* duration @ .200
.602 lift with a 1.7 rocker
Lobe B) Comp Lobe # 6580
261* duration @ .006
235* duration @ .050
153* duration @ .200
.595 lift with a 1.7 rocker
Lobe A has +24* duration at .006
Lobe A has +1* duration at .050
Lobe A has +4* duration at .200
Lobe A has .007 more total lift.
What lobe is more aggressive?
I'm about 80% sure of this from what I've read on here, experts chime in to negate or reinforce
Roller lifters don't have the same cam velocity problem, but they create sideloads on the lifter bore that the flat lifters don't, so there is a practical limit to cam velocity with rollers. too. Max Cam Velocity limits the lift you can get with a certain duration, so if you need more lift you up the RAR. Some enignes use 2.0, 2.1, 2.2 and maybe more. Those aren't engines we drive around however.
If you are at the edge of the envelope, where almost all successful racers are, you need lobes designed for the RAR you are using. It's valve motion that we are concerned about, not just lifter motion.
There's no free lunch with RAR, because a higher RAR multiplies the valve spring loads into the pushrod and lifter. So with a 2:1 RAR and 600# over the nose, the pushrod sees 1200# static and much more dynamically. No wimpy 5/16 or 3/8 pushrods here if 8000++ is your goal.
Bonus question: If you are at max lobe lift you can get, and max RAR, and still need more valve lift, what do you do? Easy answer, but tough execution.
Last edited by Old SStroker; Oct 23, 2005 at 10:42 AM.
with both cams go ahead and assume the LSA, ground in advance and other variables are the same (unless you think that would come into play)
Im not sure that there is a diff but with the smaller cam and 1.8 rockers you would have less velocity (or range of movement) on the lifters and pushrod but more pressure (i think)
And then with the bigger cam and 1.7 rockers you would have more velocity velocity (or range of movement) but less pressure on them ( i think)
Please feel free to elaborate as much as you feel like on this idea and your opinion on it, or just tell me im an idiot and it doest make a differece. Or if i stumped you, let me know so i feel good about myself.
larger base circles can be utilized since the lobe lift is down; the cam will actually 'fit' in the block since there is less of a difference in base circle size vs. lobe size; thus lowering the ratio of lobe circle/base circle; and opening possibilities for more radical ramp rates and lift numbers.
more net lift is attained as well, since in many cases the valve lash number stays the same as the ratio increases; making the valve lash effectively less in the grander scheme.
that's it, i'm all out of bullshit.
Good timing on our posts though.
Besides being a fine judge of character, per your kind words in the dynamic compression thread, you also gave the exact explanation I would have re the limits of lifter velocity and acceleration.
Re the bonus question: How do you get more lift? The same way as when you want to jump higher, you pole-vault! It's risky and tricky, but with the right stuff, at high RPM the pushrod goes 'sproing' as the acceleration turns negative approaching max lift and the valve soars 50 or 100 thous. higher than the lobe lift times RAR dictates. Then, if all goes well, the components comer back together and gently touch down on the closing flank, just like a ski jumper. (and, just like a skier that out-jumps the hill, if the landing is on the base circle, bad stuff ensues....)


