Digital Data Processing Method for Shock Tube
Abstract
We discuss a simple data acquisition system (DAQ) setup for high frequency pressure measurements in shock tube operations. The details of a new method to post-process the data using a scientific computing language to determine flow characteristics are described. The results give valuable insights into the time evolution of shocks and expansion waves in a shock tube process.
Recommended Citation
F. A. Kalany and K. M. Isaac, "Digital Data Processing Method for Shock Tube," Proceedings of the AIAA Scitech 2021 Forum (2021, Nashville, TN), pp. 1 - 9, American Institute of Aeronautics and Astronautics (AIAA), Jan 2021.
The definitive version is available at https://doi.org/10.2514/6.2021-0323
Meeting Name
AIAA Scitech 2021 Forum (2021: Jan.11-15, Nashville, TN)
Department(s)
Mechanical and Aerospace Engineering
International Standard Book Number (ISBN)
978-162410609-5
Document Type
Article - Conference proceedings
Document Version
Citation
File Type
text
Language(s)
English
Rights
© 2020 American Institute of Aeronautics and Astronautics (AIAA), All rights reserved.
Publication Date
15 Jan 2021
