AERODYNAMIC FLOW CONTROL AND ADVANCED DIAGNOSTICS (AFCAD) RESEARCH GROUP: Tools and Facilities
Tools and Facilities
Major Hardware:
- Vision Research v1210 high-speed camera, full frame at 12.7 kHz, 24GB memory
- Vision Research v311 high-speed camera, full frame at 3.25 kHz, 8GB memory
- Two pco.1600 interline transfer CCD cameras
- NewWave Solo XT, 200 mJ/pulse double-pulse PIV laser
- Quantel Evergreen Laser, 200 mJ/pulse double-pulse PIV laser
- Photonics Industries DM110 dual-cavity, high-speed Nd:YAG laser (7 mJ/pulse at 10 kHz)
- Two high-speed pressure scanners (Measurement Specialties ESP-32HD, 32 channels per brick, 1.2 kHz DAQ, +/- 30 psig)
Capabilities:
- Standard and time-resolved particle image velocimetry (PIV)
- Stereo PIV at 10 Hz
- Fast-response pressure-sensitive paint (PSP) at 5 kHz
We maintain a large fleet of UAS test vehicles for a variety of applications including:
- Flutter testing
- Multi-rotor aerodynamic interactions
- Real-time system identification and control
- Aerodynamic flow control integration
- Long-endurance dynamic soaring
Facility Specifications
- Open return wind tunnel.
- 125 hp, 3-phase AC motor with 8' (2.44 m)-diameter, 6-bladed fan (belt-driven).
- Maximum speed: 45 m/s (100 mph).
- Reynolds number up to 920,000/ft.
- Test Section: 3'x5' (0.91x1.52 m) cross-section of length 7.87' (2.4 m) with optical access on top and one side.
Contact: Prof. Matthew McCrink (mccrink.2@osu.edu)
Facility Specifications
- Blow-down wind tunnel with independent setting of Mach and Reynolds numbers.
- Capable of producing Mach number oscillations between Mach 0.4-0.6 at a controlled frequency up to 25 Hz, achieved with four counter-rotating choke bars driven by a 5-hp variable-frequency AC motor.
- Reynolds number range of 2-16 million per foot.
- Air farm consisting of two 750 cu. ft. tanks pressurized up to 2,250 psi each with air dryers.
- ±0.5% turbulence level, 15:1 contraction ratio.
- Settling chamber equipped with perforated plate, honeycomb and eight screens (60-mesh).
- Test section: 6"x22" (0.15x0.56 m) cross-section with length of 44" (1.12 m).
- Perforated sidewalls and ceiling with 1/8" holes (6% porosity) create isolated cavities for reducing Mach wave reflections in test section.
- Optical access on top and lateral sides.
Associated Instrumentation & Equipment
- Library of airfoil models designed for testing in this facility.
- Traversing wake probe.
- High-speed pressure scanners (up to 12 kHz DAQ rate).
- Hot film sensor mounted on a conical probe for insertion into test section (TSI model 1231-60W).
Contact: Prof. Matthew McCrink (mccrink.2@osu.edu)
A dedicated area for students in the research group allows quiet working conditions for days of fruitful experimental analysis. The student office is equipped with eight personal desks and desktop computers for research work. A round discussion table in the room facilitates small project meetings. The room is also equipped with a chalkboard and small refrigerator.
Students often make this area their "home away from home," keeping snacks and personal libraries here to enhance their research efforts. We keep a couple of frisbee disks on hand for "down time," sometimes leading to short games of ultimate frisbee on the back lawn of the lab.