Title

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.

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

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