Instrumentation for measuring temperature, velocity, and species concentrations in high-speed flows are critical for the development of propulsion and flight systems. The diagnostic system proposed here addresses measurement needs in a wide variety of applications in DoD facilities, national laboratories, industry, and academia. Planar measuremenets of temperature and velocity are useful in hypersonic flows, gas-turbine engines, scramjets, and pulse detonation engines, among others. Measurements of vibrational temperature are useful in non-equilibrium flows. Other applications include internal combustion engines and high-speed diesel sprays. These applications as well as follow-on work in OH PLIF, CH PLIF, acetone PLIF, and planar Doppler velocimetry are areas for significant market potential.
Potential NASA applications include measurements in ATP facilities under the auspices of the Aerothermodynamics Laboratory, such as the 31" Mach 10 facility, the 20" Mach 6 facility, the 15" Mach 6 facility, and the 20" Mach 6 CF4 facility. These facilities can utilize measurements of planar velocimetry molecular tagging velocimetry (MTV) and dual-line NO PLIF for temperature measurements. In addition, dual-line NO PLIF can be used for vibrational temperature measurements in non-equilibrium flows. The ability to track flow features at MHz rates allows detailed visualization of flow behavior, such as boundary layer separation, to aid with understanding re-entry phenomena, and for studying scramjet ignition and combustion, Finally, the Phase I will also evaluate the requirements for high frame rate (~50 kHz) imaging in high enthalpy impulse facilities, enabling ~20-30 UV or filtered Rayleigh scattering images to be obtained during single-millisecond duration "shots." The ability to capture this many planar data sets in single run would greatly enhance the productivity and reduce the cost of acquiring data in such facilities.
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