TY - JOUR
T1 - Comparing pyrometry and thermography in ballistic impact experiments
AU - Woodruff, Connor
AU - Dean, Steven W.
AU - Cagle, Colton
AU - Luke Croessmann, Charles
AU - Pantoya, Michelle L.
N1 - Funding Information:
We are thankful for support from ARO (Grant W911NF171-0387), the ONR (Grant N00014-19-1-2082), and STEM grants from the DOE (Grant DE-NA0003988) and ONR (N00014-21-1-2519). Additionally, Sandia National Laboratories is a multi-mission laboratory managed and operated by National Technology & Engineering Solutions of Sandia, LLC, a wholly owned subsidiary of Honeywell International Inc., for the U.S. Department of Energy’s National Nuclear Security Administration under contract DE-NA0003525. This paper describes objective technical results and analysis. Any subjective views or opinions that might be expressed in the paper do not necessarily represent the views of the U.S. Department of Energy or the United States Government.
Publisher Copyright:
© 2021 The Author(s)
PY - 2022/2/15
Y1 - 2022/2/15
N2 - Thermal analyses of projectile impact and subsequent combustion are investigated for aluminum projectiles using a high-velocity impact ignition system. Temperature measurements are compared using pyrometry and thermography. The implementation of these techniques is discussed, as well as their benefits and limitations in ballistic experiments. Results show pyrometry is best for measuring temperatures in the immediate vicinity surrounding the impact location, while thermography better quantifies temperature dissipation downstream from impact as the combusting debris cloud disperses. Temperatures comparable to the predicted adiabatic flame temperature are observed with the pyrometer. For thermography, emphasis is placed on the treatment of emissivity in temperature calculations. Three combustion stages are identified in the thermography data and attributed to 1) ignition and growth of the combustion front, 2) thermal dissipation due to initial particle burnout, and 3) a slower dissipation stage caused by reduced heat exchange between the burning debris cloud and surroundings.
AB - Thermal analyses of projectile impact and subsequent combustion are investigated for aluminum projectiles using a high-velocity impact ignition system. Temperature measurements are compared using pyrometry and thermography. The implementation of these techniques is discussed, as well as their benefits and limitations in ballistic experiments. Results show pyrometry is best for measuring temperatures in the immediate vicinity surrounding the impact location, while thermography better quantifies temperature dissipation downstream from impact as the combusting debris cloud disperses. Temperatures comparable to the predicted adiabatic flame temperature are observed with the pyrometer. For thermography, emphasis is placed on the treatment of emissivity in temperature calculations. Three combustion stages are identified in the thermography data and attributed to 1) ignition and growth of the combustion front, 2) thermal dissipation due to initial particle burnout, and 3) a slower dissipation stage caused by reduced heat exchange between the burning debris cloud and surroundings.
KW - Aluminum Combustion
KW - Emissivity
KW - High-Velocity Impact
KW - Optical Diagnostics
KW - Thermal Radiation
UR - http://www.scopus.com/inward/record.url?scp=85119421648&partnerID=8YFLogxK
U2 - 10.1016/j.measurement.2021.110488
DO - 10.1016/j.measurement.2021.110488
M3 - Article
AN - SCOPUS:85119421648
SN - 0263-2241
VL - 189
JO - Measurement: Journal of the International Measurement Confederation
JF - Measurement: Journal of the International Measurement Confederation
M1 - 110488
ER -