Measurements of Scramjet Fueling Conditions
Author:
Affiliation:
1. Air Force Research Laboratory
2. Innovative Scientific Solutions, Inc.
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-1360
Reference9 articles.
1. Gas property measurements in a supersonic combustor using nanosecond gated laser-induced breakdown spectroscopy with direct spectrum matching
2. Direct spectrum matching of laser-induced breakdown for concentration and gas density measurements in turbulent reacting flows
3. Simultaneous gas density and fuel concentration measurements in a supersonic combustor using laser induced breakdown
4. Raman scattering measurements of mixing and finite-rate chemistry in a supersonic reacting flow over a piloted, ramped cavity
5. Dual-Pump CARS Measurements in the University of Virginia's Dual-Mode Scramjet: Configuration "A"
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1. Numerical Simulation of Multi-Component Flows with Variable Thermodynamic Properties Towards Supersonic Flow Over a Cavity;AIAA SCITECH 2024 Forum;2024-01-04
2. Effect of fuel temperature on mixing characteristics of a kerosene jet injected into a cavity-based supersonic combustor;Physics of Fluids;2023-04-01
3. Development of a fs/ps CARS system for temperature and species measurements in a dual-mode scramjet combustor;AIAA SCITECH 2023 Forum;2023-01-19
4. Ignition dynamics of a pulse detonation igniter in a supersonic cavity flameholder;Combustion and Flame;2020-05
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