Shock tube and gas dynamic design considerations and implementation for extended test times
Author:
Affiliation:
1. University of Central Florida
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2023-3028
Reference21 articles.
1. Characterization of a new ultra-high pressure shock tube facility for combustion and propulsion studies
2. Shock tube investigation of high-temperature, extremely-rich oxidation of several co-optima biofuels for spark-ignition engines
3. Reflected shock-initiated ignition probed via simultaneous lateral and endwall high-speed imaging with a transparent, cylindrical test-section
4. A comprehensive experimental and kinetic modeling study of 1- and 2-pentene
5. Time-resolved measurements of key intermediate products during cyclopentanone pyrolysis in a shock tube
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