TY - GEN
T1 - Low-cost arduino-based data acquisition system with android mobile interface for undergraduate aerodynamics laboratories
AU - Schwaab, Quentin
AU - Belleau, Christian
AU - Morency, François
AU - Weissx, Julien
N1 - Publisher Copyright:
© 2016, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2016
Y1 - 2016
N2 - A mobile application has been developed using the Android Studio Integrated Development Environment to interface over Bluetooth with an inexpensive, Arduino-based data acquisition module. The system is implemented for wireless pressure and temperature measurements in the context of undergraduate aerodynamics laboratories. Essentially, it allows to remotely select a sensor, retrieve a given number of samples at a desired sampling rate, stream data to a real-time graph and save the results into a file. The designed DAQ system, whose total cost is less than $100, includes an Arduino microcontroller, a Bluetooth module, two pressure sensors and a temperature probe. To validate the system, mean velocity profiles are carried out in an open-jet wind tunnel using a Pitot-static tube. Despite a relatively limited signal resolution, the results match very well the ones obtained with more advanced instrumentation.
AB - A mobile application has been developed using the Android Studio Integrated Development Environment to interface over Bluetooth with an inexpensive, Arduino-based data acquisition module. The system is implemented for wireless pressure and temperature measurements in the context of undergraduate aerodynamics laboratories. Essentially, it allows to remotely select a sensor, retrieve a given number of samples at a desired sampling rate, stream data to a real-time graph and save the results into a file. The designed DAQ system, whose total cost is less than $100, includes an Arduino microcontroller, a Bluetooth module, two pressure sensors and a temperature probe. To validate the system, mean velocity profiles are carried out in an open-jet wind tunnel using a Pitot-static tube. Despite a relatively limited signal resolution, the results match very well the ones obtained with more advanced instrumentation.
UR - https://www.scopus.com/pages/publications/84979978253
U2 - 10.2514/6.2016-4323
DO - 10.2514/6.2016-4323
M3 - Contribution to conference proceedings
AN - SCOPUS:84979978253
SN - 9781624104381
T3 - 32nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference
SP - 1
EP - 15
BT - 32nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - 32nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference, 2016
Y2 - 13 June 2016 through 17 June 2016
ER -