Anyone with some downforce knowledge?
#1
Anyone with some downforce knowledge?
Ok , so using this formula
http://en.wikipedia.org/wiki/Downforce <-- wont copy paste .
I'm trying to find what the angle of attack should be on a wing .
according to this http://en.wikipedia.org/wiki/Angle_of_attack
the problem is on a car's wing the angle of attack is the opposite as shown here . so does that mean that it would be negative angle ,
for example .. if said wing is said to have 15 degrees angle . how would you plot that into the equation ?
as a 15* ?? do you plot it as a decimal .54, fraction ? 360/15 ? is it negative since the angle is opposite as to what it shown for aircraft which is where normally the equation is used for ?
http://en.wikipedia.org/wiki/Downforce <-- wont copy paste .
I'm trying to find what the angle of attack should be on a wing .
according to this http://en.wikipedia.org/wiki/Angle_of_attack
the problem is on a car's wing the angle of attack is the opposite as shown here . so does that mean that it would be negative angle ,
for example .. if said wing is said to have 15 degrees angle . how would you plot that into the equation ?
as a 15* ?? do you plot it as a decimal .54, fraction ? 360/15 ? is it negative since the angle is opposite as to what it shown for aircraft which is where normally the equation is used for ?
Last edited by Tem120; 10-02-13 at 10:52 AM.
#2
Wastegate John
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The angle of attack is dependant on the conditions and the desired amount of downforce.
The manufacturer should have that info available to you if they are any good.
Example: APR APR Performance - GTC-300 - CFD Data & Analysis
The manufacturer should have that info available to you if they are any good.
Example: APR APR Performance - GTC-300 - CFD Data & Analysis
#3
The angle of attack is dependant on the conditions and the desired amount of downforce.
The manufacturer should have that info available to you if they are any good.
Example: APR APR Performance - GTC-300 - CFD Data & Analysis
The manufacturer should have that info available to you if they are any good.
Example: APR APR Performance - GTC-300 - CFD Data & Analysis
it also gives CL , per setting , at 15* it has -.075 CL so if at 15* its at that would it be redundant to plug the angle of attack again since it was already calculated into the lift coefficiency ?
Last edited by Tem120; 10-02-13 at 11:25 AM.
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