- #1
Ittiandro
- 54
- 3
Hi!
I know little about physics, but I am very well educated , with an inquisitive mind.
First the context, then my specific question
A. Context
The practice of windsurfing has brought me to try and understand the principles of hydrodynamics, in order to make my sailing more efficient.
As explained below , in this post I am enquiring on the fluid viscosity issue, more particularly about the Reynolds number .
I am currently working on a prototype of a DIY hydrofoil wing to attach to my windsurfing board, as per photo.
Currently, these hydrofoil wings are commercially available, but very expensive, because made in carbon. This is why I was thinking to make one myself either in plastic, fiberglas or other suitable material using a 3D printer., or even in fiberglas-reinforced wood , to be shaped by hand.
Windsurfing experts, who are not necessarily trained in physics, say that the mechanical stress on the hydrofoil wing moving through a relatively dense ( viscous) medium like water, is such that it can break the housing of the wing, particularly the one of my board, which is not designed for speed and high performance and isn’t therefore strong enough to withstand the mechanical stress.
B. Question
The reason why I am bringing up this issue in your Forum is that I can’t understand why a windsurfing board moving in water at only 18-20 knts/hr , can create such a mechanical stress on the hydrofoil wing as to rip it off the fin housing..at the bottom of the hull.
As an experiment, I tried to push, pull and twist ( with moderate force) on the fin ( and the housing) , but the fin box withstood the action pretty well. I would have probably succeeded in breaking or damaging it by applying full strength or leaning on the fin with half (or even all) of my body weight , which means at least at least 40 kg, but I can’t see how a 40 kg force can be exerted on the hydrofoil wing , simply on account of the water resistance: the hydrodynamic flow of water encountering the leading edge of the moving wing is not orthogonal to the its surface,( in which case I would perhaps understand ) but practically parallel, as it follows the curved chord of the wing cross section. More specifically, my question is :
Can this alleged stress ( or force) be measured, in kg/cm2 of surface, once we know the angle of attack of the wing., its surface , thickness, the density /viscosity of water at a given temperature.?
Can it be calculated from the Reynolds number?
I discovered that there is a number called Reynolds number, expressing, as I understand, the viscosity coefficient of water or air in function of the velocity of the wing foil, the density of the medium,(air or water) the length of the wing chord and the temperature .
I googled up this number at http://airfoiltools.com/calculator/...0.2&MReNumForm[kvisc]=9.7937E-7&yt0=Calculate
This site has a calculator. To obtain the Reynold number , it is sufficient to enter the data in the calculator and click on the button.
For a hydrofoil having a wing chord of 0.20 m( or about 8”), moving in 20° C water at 20 knts/hr, the Reynolds number is 2,042,129.
Since the viscosity of a medium resists the movement of a body through it ( and can therefore be viewed as a force exerted on it) , I wonder if there is a formula allowing to extract this force ( kg/cm2) from the Reynolds number .
For some reasons, to obtain the Reynolds number, one is not required to provide the length( wingspan) of the wing, neither does the thickness enter into its calculation.
If necessary, let’s assume the length to be 28”, i. e.t the wing has the shape of a rectangle of 8” x28”, from which the surface can be derived. This would be the approximate dimension of my hydrofoil wing.
As to the thickness, if required, we can assume that it varies between 0.50 “ at the leading edge( center wing) to about 1/8” at the trailing edge and at the tips, since the wing tapers down both crosswise and lengthwise.
The angle of attack of the wing, i.e. its pitch is 0 ( zero) because the hydrodynamic flow of water encountering the leading edge of the wing is not orthogonal to the wing surface, but practically parallel to it as it follows the curved chord of the wing cross section. Possibly the drag may have to be taken into consideration, too, but for me all this would be too complicated.
Perhaps a physicist can do it relatively easily, unless there are some missing data.
At worst, the board may not lift above the water, but I am willing to try my project if I have sufficient reasons to believe that , on the basis of the estimated load in kg/cm2 extracted from the Reynolds number, these forces are not great enough to break anything..
Or am I am perhaps asking the wrong question or a question that cannot be answered? I hope not..Thanks for your help
Ittiandro
I know little about physics, but I am very well educated , with an inquisitive mind.
First the context, then my specific question
A. Context
The practice of windsurfing has brought me to try and understand the principles of hydrodynamics, in order to make my sailing more efficient.
As explained below , in this post I am enquiring on the fluid viscosity issue, more particularly about the Reynolds number .
I am currently working on a prototype of a DIY hydrofoil wing to attach to my windsurfing board, as per photo.
Currently, these hydrofoil wings are commercially available, but very expensive, because made in carbon. This is why I was thinking to make one myself either in plastic, fiberglas or other suitable material using a 3D printer., or even in fiberglas-reinforced wood , to be shaped by hand.
Windsurfing experts, who are not necessarily trained in physics, say that the mechanical stress on the hydrofoil wing moving through a relatively dense ( viscous) medium like water, is such that it can break the housing of the wing, particularly the one of my board, which is not designed for speed and high performance and isn’t therefore strong enough to withstand the mechanical stress.
B. Question
The reason why I am bringing up this issue in your Forum is that I can’t understand why a windsurfing board moving in water at only 18-20 knts/hr , can create such a mechanical stress on the hydrofoil wing as to rip it off the fin housing..at the bottom of the hull.
As an experiment, I tried to push, pull and twist ( with moderate force) on the fin ( and the housing) , but the fin box withstood the action pretty well. I would have probably succeeded in breaking or damaging it by applying full strength or leaning on the fin with half (or even all) of my body weight , which means at least at least 40 kg, but I can’t see how a 40 kg force can be exerted on the hydrofoil wing , simply on account of the water resistance: the hydrodynamic flow of water encountering the leading edge of the moving wing is not orthogonal to the its surface,( in which case I would perhaps understand ) but practically parallel, as it follows the curved chord of the wing cross section. More specifically, my question is :
Can this alleged stress ( or force) be measured, in kg/cm2 of surface, once we know the angle of attack of the wing., its surface , thickness, the density /viscosity of water at a given temperature.?
Can it be calculated from the Reynolds number?
I discovered that there is a number called Reynolds number, expressing, as I understand, the viscosity coefficient of water or air in function of the velocity of the wing foil, the density of the medium,(air or water) the length of the wing chord and the temperature .
I googled up this number at http://airfoiltools.com/calculator/...0.2&MReNumForm[kvisc]=9.7937E-7&yt0=Calculate
This site has a calculator. To obtain the Reynold number , it is sufficient to enter the data in the calculator and click on the button.
For a hydrofoil having a wing chord of 0.20 m( or about 8”), moving in 20° C water at 20 knts/hr, the Reynolds number is 2,042,129.
Since the viscosity of a medium resists the movement of a body through it ( and can therefore be viewed as a force exerted on it) , I wonder if there is a formula allowing to extract this force ( kg/cm2) from the Reynolds number .
For some reasons, to obtain the Reynolds number, one is not required to provide the length( wingspan) of the wing, neither does the thickness enter into its calculation.
If necessary, let’s assume the length to be 28”, i. e.t the wing has the shape of a rectangle of 8” x28”, from which the surface can be derived. This would be the approximate dimension of my hydrofoil wing.
As to the thickness, if required, we can assume that it varies between 0.50 “ at the leading edge( center wing) to about 1/8” at the trailing edge and at the tips, since the wing tapers down both crosswise and lengthwise.
The angle of attack of the wing, i.e. its pitch is 0 ( zero) because the hydrodynamic flow of water encountering the leading edge of the wing is not orthogonal to the wing surface, but practically parallel to it as it follows the curved chord of the wing cross section. Possibly the drag may have to be taken into consideration, too, but for me all this would be too complicated.
Perhaps a physicist can do it relatively easily, unless there are some missing data.
At worst, the board may not lift above the water, but I am willing to try my project if I have sufficient reasons to believe that , on the basis of the estimated load in kg/cm2 extracted from the Reynolds number, these forces are not great enough to break anything..
Or am I am perhaps asking the wrong question or a question that cannot be answered? I hope not..Thanks for your help
Ittiandro