Particle Image Velocimetry Measurements of Unsteady Exhaust from a Linearized Continuous Detonation Combustor
Author:
Affiliation:
1. National University of Singapore
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2023-1106
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1. Rotating Detonation Wave Propulsion: Experimental Challenges, Modeling, and Engine Concepts
2. Overview of Performance, Application, and Analysis of Rotating Detonation Engine Technologies
3. Recent Progress, Development Trends, and Consideration of Continuous Detonation Engines
4. Supersonic combustion induced by reflective shuttling shock wave in fan-shaped two-dimensional combustor
5. Investigation of combustion modes and pressure of reflective shuttling detonation combustor
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