Need help figuring Volumetric Flow of my system (fuel).
#1
10 Second Club
Thread Starter
iTrader: (9)
Join Date: Jan 2004
Location: Laconia, NH
Posts: 3,878
Likes: 0
Received 0 Likes
on
0 Posts
![Default](https://ls1tech.com/forums/images/icons/icon1.gif)
I need to figure out what my new fuel sytem is going to flow in GPM or GPS. I have the Orfice size, fuel PSI, and Specific Gravity but....I suck at math. ![Shiner](https://ls1tech.com/forums/images/smilies2/shiner.gif)
Anyone have any equations that can give me a relativly accurate answer? And no, I'm not buying a $300 flow meter.
Thanks,
Andrew
![Shiner](https://ls1tech.com/forums/images/smilies2/shiner.gif)
Anyone have any equations that can give me a relativly accurate answer? And no, I'm not buying a $300 flow meter.
Thanks,
Andrew
#3
10 Second Club
Thread Starter
iTrader: (9)
Join Date: Jan 2004
Location: Laconia, NH
Posts: 3,878
Likes: 0
Received 0 Likes
on
0 Posts
![Default](https://ls1tech.com/forums/images/icons/icon1.gif)
The orfice size is .056", 60psi, .733 specific gravity. Now I asume SG can be substituted for Density. I ran the numbers through an orfice flow rate calculator I found on a Fluid Dynamics website and it came out to almost 3GPM, seems real high to me.
Any help would be awesome.
Andrew
Any help would be awesome.
Andrew
#5
10 Second Club
Thread Starter
iTrader: (9)
Join Date: Jan 2004
Location: Laconia, NH
Posts: 3,878
Likes: 0
Received 0 Likes
on
0 Posts
![Default](https://ls1tech.com/forums/images/icons/icon1.gif)
I'm just trying to get a general idea of consumption. I'm figuring 60psi on the high side, it will realistically be 2-3lbs lower. Basicly, I think my fuel cell is way to small for going out to street night. Holds less than a gallon and looking at the design, I think I'm going to see cavitation problems on launch once it gets down to a 1/3 full.
#6
TECH Enthusiast
iTrader: (2)
Join Date: Feb 2002
Location: Elk Grove, IL
Posts: 610
Likes: 0
Received 0 Likes
on
0 Posts
![](https://ls1tech.com/forums/images/ranks/ls1tech10year.png)
![Default](https://ls1tech.com/forums/images/icons/icon1.gif)
specific gravity is a ratio of the density of the fluid to the denisty of water. Water is 62.4 lb/ft^3 so that means the density of your gasoline is (62.4)(.733)= 45.74 lb/ft^3
Trending Topics
#8
10 Second Club
Thread Starter
iTrader: (9)
Join Date: Jan 2004
Location: Laconia, NH
Posts: 3,878
Likes: 0
Received 0 Likes
on
0 Posts
![Default](https://ls1tech.com/forums/images/icons/icon1.gif)
After doing my home work, I'm doing this all wrong. I'm working with two jets and that gets complicated as per http://www.nescaracing.com/n2o.html . The two jets are .028. So it looks like I need to find the total area of the two.
Here's the formula I found for open flow testing.
Fuel Jet Diameter X Fuel Jet Diameter X .7854 X Number of Jets = Flow test jet area
(Flow test jet area / .7854)SqRt = Flow jet size in thousandths
Now, here's the formula for fuel flow through orfice.
Q = Ao Co (( 2 x Pd / p)SqRt)
Where:
Q - Flow rate in cubic meters per second
Ao - Area of orifice (fuel jet) in square meters
Co- Flow Coefficient of orifice (use .75 as an approximation of Reynolds formula)
Pd - Pressure Differential between inlet and outlet of orifice (6-7lbs)
p - fuel specific gravity (kg/ cu meter - multiply spec gravity by 1000 for metric equiv)
I'll have to sit down and figure this out later when I have the time to do all the conversions.
JL, I have the all the jets I need for a high pressure set up, so I really wasn't going to go with a low PSI set up unless I have tuning issues. I don't see why I would have any issues.
#9
Race your car!
iTrader: (50)
![Default](https://ls1tech.com/forums/images/icons/icon1.gif)
I understand where you're coming from now. I don't think you'll have issues, I just haven't heard of too many people that go about it that way. You can still adjust the fuel flow with pressure, but at high pressure a 1/2 lb adjustment is probably very hard to get, and with the higher pressure a pressure change probably makes more of a difference.
#12
10 Second Club
Thread Starter
iTrader: (9)
Join Date: Jan 2004
Location: Laconia, NH
Posts: 3,878
Likes: 0
Received 0 Likes
on
0 Posts
![Default](https://ls1tech.com/forums/images/icons/icon1.gif)
Well I came up with .324 GPM using this calculator http://www.efunda.com/formulae/fluid...meter.cfm#calc . So I would probably use about 1/2 gallon a night. I believe my stand alone only holds .8 gallons and, as I mentioned the pump is in the cell, with no baffles, sort of angled twards the front corner of the car. I think I might sell this one and get a 1 gallon sumped tank with an external pump.
#13
TECH Senior Member
iTrader: (2)
![Default](https://ls1tech.com/forums/images/icons/icon1.gif)
Thanks for the info.
After doing my home work, I'm doing this all wrong. I'm working with two jets and that gets complicated as per http://www.nescaracing.com/n2o.html . The two jets are .028. So it looks like I need to find the total area of the two.
Here's the formula I found for open flow testing.
Fuel Jet Diameter X Fuel Jet Diameter X .7854 X Number of Jets = Flow test jet area
(Flow test jet area / .7854)SqRt = Flow jet size in thousandths
Now, here's the formula for fuel flow through orfice.
Q = Ao Co (( 2 x Pd / p)SqRt)
Where:
Q - Flow rate in cubic meters per second
Ao - Area of orifice (fuel jet) in square meters
Co- Flow Coefficient of orifice (use .75 as an approximation of Reynolds formula)
Pd - Pressure Differential between inlet and outlet of orifice (6-7lbs)
p - fuel specific gravity (kg/ cu meter - multiply spec gravity by 1000 for metric equiv)
I'll have to sit down and figure this out later when I have the time to do all the conversions.
JL, I have the all the jets I need for a high pressure set up, so I really wasn't going to go with a low PSI set up unless I have tuning issues. I don't see why I would have any issues.
After doing my home work, I'm doing this all wrong. I'm working with two jets and that gets complicated as per http://www.nescaracing.com/n2o.html . The two jets are .028. So it looks like I need to find the total area of the two.
Here's the formula I found for open flow testing.
Fuel Jet Diameter X Fuel Jet Diameter X .7854 X Number of Jets = Flow test jet area
(Flow test jet area / .7854)SqRt = Flow jet size in thousandths
Now, here's the formula for fuel flow through orfice.
Q = Ao Co (( 2 x Pd / p)SqRt)
Where:
Q - Flow rate in cubic meters per second
Ao - Area of orifice (fuel jet) in square meters
Co- Flow Coefficient of orifice (use .75 as an approximation of Reynolds formula)
Pd - Pressure Differential between inlet and outlet of orifice (6-7lbs)
p - fuel specific gravity (kg/ cu meter - multiply spec gravity by 1000 for metric equiv)
I'll have to sit down and figure this out later when I have the time to do all the conversions.
JL, I have the all the jets I need for a high pressure set up, so I really wasn't going to go with a low PSI set up unless I have tuning issues. I don't see why I would have any issues.
(.71 x size of one jet) X = single jet of same area
Then area is a breeze, and am sure you have that math.
Man I love this stuff, but have to go and can't get back for a while.
![Bang Head](https://ls1tech.com/forums/images/smilies/LS1Tech/gr_banghead.gif)
Robert
#14
Restricted User
iTrader: (17)
![Default](https://ls1tech.com/forums/images/icons/icon1.gif)
can this same calculator be used to calculate nitrous oxide consumption? I have been looking for something like this to calculate the actual difference in volume of say a 100 shot(pill/jet) at 1000 psi vs the same 100 shot at 1300 psi. How much more volume do you get from the additional 300 psi? Would it be close to 30% more or is it not that big of a difference?