Hypersonic Wind Tunnel
The hypersonic wind tunnel project was inspired by the NASA's arc-jet facility and was my personal attempt at creating something that could simulate similar conditions from hardware store parts in my garage. The main principle was to expand air to hundreds of times its original volume through a convergent-divergent nozzle and convert as much of its pressure energy into velocity. The high pressure ratio required meant a vacuum tank was needed to prevent flow separation and not use pressures beyond that of a high-end shop compressor. This expansion also led to significant cooling and required a heat source, and in this case it used a miniaturized arc jet to superheat the air with a confined electrical arc. Shockwaves were then visualized using Schlieren imaging to see the density gradients within the test chamber through optical glass windows. To minimize system cost and footprint, all tests only lasted about 100 milliseconds before the pressure difference became insufficient for hypersonic flow.
Test Images
This silly experiment was to test complex shock interactions on streamlined bodies, such as my go-kart with numerous fins and protrusions that would produce shockwaves.
This model rocket was a 2D cutout intended to see shockwave interactions between the nose and fin shocks, with the sharp nose point giving a refrence shockwave angle to measure test mach.
This test was designed to test the formation of bow shocks, and used a simple cylindrical test article with a 3mm nose radius.
Arc Jet SystemÂ
The arc jet system was necessary for preventing the air from liquefying due to expansion and used an electrode built into the convergent section of the nozzle. This used 15000 volts to turn the air into a plasma (the bright part of the image) and allow the air to reach full velocity, creating conditions similar to the last phase of orbital re-entry when vehicle speed drops below Mach 5.
Shockwave Visualization
All tests were captured using a Schlieren imaging apparatus in the shadowgraph configuration (circular filtering aperature vs. knife edge) for defined shockwaves in all directions with the brightness and contrast adjustable by using a small LED point source with a dimmer. The primary reflector was reused from a small telescope and the camera was my cell phone recording in slow motion (120 fps)
Schlieren imaging setup with point source (left), spherical concave mirror (right), test chamber (center), cell phone camera (left)
simplified plumbing schematic