Digital Data Processing Method for Shock Tube

Frank A. Kalany; Kakkattukuzhy M. Isaac

doi:10.2514/6.2021-0323

Digital Data Processing Method for Shock Tube

Frank A. Kalany
, Kakkattukuzhy M. Isaac

Mechanical and Aerospace Engineering

Research output: Contribution to journal › Article › peer-review

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.

Original language	American English
Journal	Proceedings of the AIAA Scitech 2021 Forum (2021, Nashville, TN)
DOIs	https://doi.org/10.2514/6.2021-0323
State	Published - Jan 15 2021

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Aerospace Engineering

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https://doi.org/10.2514/6.2021-0323

Cite this

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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.",

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AB - 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.

UR - https://scholarsmine.mst.edu/mec_aereng_facwork/4697

UR - https://doi.org/10.2514/6.2021-0323

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JO - Proceedings of the AIAA Scitech 2021 Forum (2021, Nashville, TN)

JF - Proceedings of the AIAA Scitech 2021 Forum (2021, Nashville, TN)

ER -

Digital Data Processing Method for Shock Tube

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