Small-Scale Subsonic Wind Tunnel

Independent Capstone | Solo Design, Build and Test | Autodesk Inventor | FDM Printing | Mar–May 2026

← Back to Projects
CAD assembly
CAD assembly
Assembled tunnel and plenum
Assembled tunnel and plenum
The 82L plenum that failed
The 82L plenum that failed
Final 22L plenum
Final 22L plenum
Before velvet fabric: glare
Before velvet fabric: glare
After velvet fabric: glare reduced
After velvet fabric: glare reduced
Why

Wind tunnels in Indonesia sit in a handful of institutions, so most engineering students, me included, never test anything in one. I set out to build a desktop tunnel that students could afford to design and build; about a metre long, at least 7 m/s wind velocity through the test section, under Rp 2.5 million. This wind tunnel is purely for educational purposes, for students to understand how air flows through object.

The problem

I was building every part alone, on a BambuLab X1 3D Printer with a 257 mm bed, and in a wind tunnel every part affects the flow. Most of the real problems only showed up once the parts existed and tested.

#
What went wrong
What I changed
01
What went wrong

The planned 20 × 20 cm test section was as wide as the 225 mm fan, leaving the diffuser with nothing to expand into and its inlet wouldn't fit the print bed even in four pieces.

What I changed

Cut the test section to 15 × 15 cm and re-derived the geometry from the contraction ratio: 7.1, inside the recommended 6-9 ratio, on a fifth-order polynomial contour.

02
What went wrong

Water vapour, the original smoke source, was far too thin for the volume of air a 225 mm fan moves.

What I changed

Switched to a fog machine running a glycerine-aquadest mix.

03
What went wrong

The 82 L plenum lost pressure and heat so fast that the smoke settled on the floor of the box.

What I changed

Rebuilt it at 22 L. When that was still too thin, shortened the delivery hose and moved the valve.

04
What went wrong

The short copper tubes for the smoke rake slipped in the bender and kinked: they folded flat at the bend instead of curving.

What I changed

Printed a PLA clamping block for the die that pins the tube, giving a clean, even bend.

05
What went wrong

The drilled reservoir holes choked the smoke on its way into the rake.

What I changed

Opened them into one rectangular slot. The tubes were already held by the rake mount, so the holes weren't structural.

06
What went wrong

The black-painted test chamber reflected the LED light and washed out the streamlines.

What I changed

Lined the walls and floor with velvet fabric, which absorbs the light and gives a dark background with significantly reduced glare.

The result

Six of seven specifications met. The tunnel draws clear, steady streamlines around an airfoil at about 80 % fan speed, runs on 65 W from a household socket, and is now in use as a university fluid mechanics lab instrument. It came in 3.6 % over budget because trial and error resulted in more filament used. Validation was visual: 7.42 m/s is calculated from the fan's rated flow and the honeycomb blockage and measuring it with a pitot tube is the next step.

7.1
Contraction ratio
7.42 m/s
Test section, calculated
65 W
Fan power
6 / 7
Specifications met
In use
University lab
With the finished tunnel
With the finished tunnel
Demonstration to students
Demonstration to students