Time-Resolved Stagnation Pressure Measurement Technique in a Rotating Detonation Rocket Combustor
Author:
Affiliation:
1. Purdue University
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2023-1871
Reference25 articles.
1. Pressure measurement by fast-response piezo-electric sensors during continuous spin detonation in the combustor
2. Self-Excited, Multi-kHz Dynamics in a Linear, Semi-Bounded Detonation Channel
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