How to build a simple wind tunnel force balance?

AI Thread Summary
A user has built a wind tunnel with a 15 x 15 in. test section and seeks advice on creating a simple force balance to measure lift and drag forces simultaneously. Currently, they use a single-axis load cell for drag measurement and are exploring options for measuring lift, such as additional load cells or strain gauges. Suggestions include using an L-bar pivot system to isolate drag forces, but this setup only measures drag. To measure lift, alternatives like a weighing scale or multiple load cells calibrated on a platform are proposed. The user emphasizes the need for sufficient accuracy to plot coefficients of lift and drag against the angle of attack for educational experiments.
foxkilo
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I have constructed a wind tunnel with approximately 15 x 15 in. cross-sectional area test section.

Where can i get some ideas/plans to build a simple force balance that can measure lift and drag forces simultaneously?

Currently I'm using a single-axis button load-cell setup to measure drag. How to design a mounting solution for another load cell to measure the lift force? Or there are much better ways of doing this, e.g. using strain gauges? :confused:

Need not be too accurate; this tunnel is intended for educational purposes only. Any help is appreciated, thanks.
 
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foxkilo said:
Need not be too accurate; this tunnel is intended for educational purposes only. Any help is appreciated, thanks.

:rolleyes:
hang the model from a spring scale
 
OK, I need enough accuracy to run experiments such as plotting CL and CD vs. angle of attack. :biggrin:

I'm trying to use load cells or strain gauges that can be hooked up to digital readouts.

Need some mechanical contraption that can isolate the lift and drag forces as much as possible...??

Like for example, I'm currently using an L-bar pivoting at the intersection of the L, model mounted on the tip of the longer end of the "L", and load cell placed under the short end. Drag forces pull the model back, the L-bar pivots and applies a load to the load cell... But this method only measures DRAG... so I have a one-trick pony here...
 
Obviously, you ll be putting this L section somewhere, just put a weighing scale below it, difference in weight gives u the lift.

Again if size of the weighing scale is an issue, you can use a platform & use load cells below it(at least three, & of course a bit of calibration), to see the vertical force.

hey, may I know what does the model look like?
 
foxkilo said:
OK, I need enough accuracy to run experiments such as plotting CL and CD vs. angle of attack. :biggrin:

I'm trying to use load cells or strain gauges that can be hooked up to digital readouts.

Need some mechanical contraption that can isolate the lift and drag forces as much as possible...??

Like for example, I'm currently using an L-bar pivoting at the intersection of the L, model mounted on the tip of the longer end of the "L", and load cell placed under the short end. Drag forces pull the model back, the L-bar pivots and applies a load to the load cell... But this method only measures DRAG... so I have a one-trick pony here...

What type of load cell are you using because I am trying to preform a project to reduce drag on airplane wings using winglets?
 
Due to the constant never ending supply of "cool stuff" happening in Aerospace these days I'm creating this thread to consolidate posts every time something new comes along. Please feel free to add random information if its relevant. So to start things off here is the SpaceX Dragon launch coming up shortly, I'll be following up afterwards to see how it all goes. :smile: https://blogs.nasa.gov/spacex/
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