Laser diagnostics on a hypersonic combustor
Conference
·
OSTI ID:6120465
- Los Alamos National Laboratory, NM (USA) NASA, Langley Research Center, Hampton, VA (USA)
NASA-Langley has implemented a laser-based multipoint/multiparameter diagnostics system at its hypersonic direct-connect combustor, in order to measure both temperature and majority species densities in two dimensions, using spatially-scanned CARS; in addition, line-imaged measurements of radical densities are simultaneously generated by LIF at any of several planes downstream of the fuel injector. Initial experimental trials have demonstrated successful detection of one-dimensional images of OH density, as well as CARS N2-temperature measurements, in the turbulent reaction zone of the hypersonic combustor.
- OSTI ID:
- 6120465
- Report Number(s):
- AIAA-Paper-91-0456; CONF-910117-
- Resource Relation:
- Conference: 29. AIAA aerospace sciences conference, Reno, NV (USA), 7-10 Jan 1991
- Country of Publication:
- United States
- Language:
- English
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Related Subjects
33 ADVANCED PROPULSION SYSTEMS
COMBUSTORS
DIAGNOSTIC TECHNIQUES
CHEMICAL REACTION YIELD
COMBUSTION
COMBUSTION KINETICS
COMBUSTION PRODUCTS
FUEL INJECTION SYSTEMS
HYDROXYL RADICALS
HYPERSONIC FLOW
JETS
MIXING
RAMAN SPECTRA
WIND TUNNELS
CHEMICAL REACTION KINETICS
CHEMICAL REACTIONS
FLUID FLOW
FUEL SYSTEMS
KINETICS
OXIDATION
RADICALS
REACTION KINETICS
SPECTRA
THERMOCHEMICAL PROCESSES
TUNNELS
UNDERGROUND FACILITIES
YIELDS
330603* - Vehicle Design Factors- Engine System
COMBUSTORS
DIAGNOSTIC TECHNIQUES
CHEMICAL REACTION YIELD
COMBUSTION
COMBUSTION KINETICS
COMBUSTION PRODUCTS
FUEL INJECTION SYSTEMS
HYDROXYL RADICALS
HYPERSONIC FLOW
JETS
MIXING
RAMAN SPECTRA
WIND TUNNELS
CHEMICAL REACTION KINETICS
CHEMICAL REACTIONS
FLUID FLOW
FUEL SYSTEMS
KINETICS
OXIDATION
RADICALS
REACTION KINETICS
SPECTRA
THERMOCHEMICAL PROCESSES
TUNNELS
UNDERGROUND FACILITIES
YIELDS
330603* - Vehicle Design Factors- Engine System