Transactions of Nanjing University of Aeronautics & Astronautics
Archive > Volume 37 Issue 1 > 2020,37(1):155-163. DOI:10.16356/j.1005-1120.2020.01.014 Prev Next

Design and Experiment of Streamlined Piezoelectric Pump with Low Vortex and Large Flow Rate

CHINA AERO-SCIENCES

WeChat

Mobile website