TY - GEN
T1 - Force measurement system of a low-speed wind tunnel
AU - Yan, Li
AU - Xingzhi, Ding
AU - Yankui, Wang
PY - 2009
Y1 - 2009
N2 - Wind tunnel is a basic experimental facility, in which a variety of aerodynamic research can be conducted by measuring force acted on the test model, pressure distribution on the model surface, as well as by visualizing the flow around the model. The force measurement test is conventional and especially important for the aircraft and other vehicle design to predict their performance. The force measurement system of D-4 wind tunnel in Beijing University of Aeronautics and Astronautics is introduced together with a force measurement test as an instance.
AB - Wind tunnel is a basic experimental facility, in which a variety of aerodynamic research can be conducted by measuring force acted on the test model, pressure distribution on the model surface, as well as by visualizing the flow around the model. The force measurement test is conventional and especially important for the aircraft and other vehicle design to predict their performance. The force measurement system of D-4 wind tunnel in Beijing University of Aeronautics and Astronautics is introduced together with a force measurement test as an instance.
KW - Data acquisition and processing
KW - Force measurement system
KW - Strain gauge balance
KW - Wind tunnel
UR - https://www.scopus.com/pages/publications/71549173156
U2 - 10.1109/ICEMI.2009.5274309
DO - 10.1109/ICEMI.2009.5274309
M3 - 会议稿件
AN - SCOPUS:71549173156
SN - 9781424438624
T3 - ICEMI 2009 - Proceedings of 9th International Conference on Electronic Measurement and Instruments
SP - 3302
EP - 3305
BT - ICEMI 2009 - Proceedings of 9th International Conference on Electronic Measurement and Instruments
T2 - 9th International Conference on Electronic Measurement and Instruments, ICEMI 2009
Y2 - 16 August 2009 through 19 August 2009
ER -