Article
Digital Data Processing Method for Shock Tube
Proceedings of the AIAA Scitech 2021 Forum (2021, Nashville, TN)
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.
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
1-15-2021
Publication Date
15 Jan 2021
Disciplines
Citation Information
Frank A. Kalany and Kakkattukuzhy M. Isaac. "Digital Data Processing Method for Shock Tube" Proceedings of the AIAA Scitech 2021 Forum (2021, Nashville, TN) (2021) p. 1 - 9 Available at: http://works.bepress.com/kakkattukuzhy-isaac/46/