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Raman shifting a tunable ArF excimer laser to wavelengths of 190 to 240 nm with a forced convection Raman cell by Balla, R. Jeffrey
Published 2000Call Number: Loading…
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Planar Rayleigh scattering and laser-induced fluorescence for visualization of a hot, Mach 2 annular air jet by Balla, R. Jeffrey
Published 1994Call Number: Loading…
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3
Iodine Tagging Velocimetry and mechanism in the hypersonic near wake of a MultiPurpose Crew Vehicle / by Balla, R. Jeffrey
Published 2013Call Number: Loading…Online Access
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Government Document eBook -
4
Raman shifting a tunable ArF excimer laser to wavelengths of 190 to 240 nm with a forced convection Raman cell / by Balla, R. Jeffrey, Herring, Gregory C.
Published 2000Call Number: Loading…Online Access
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5
Freestream Mach-number and temperature measurement in NASA Langley's 20-inch supersonic wind tunnel using laser-induced thermal acoustics / by Herring, Gregory C., Balla, R. Jeffrey, Beeler, George B.
Published 2020Call Number: Loading…Online Access
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Government Document eBook
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Related Subjects
Argon
Fluorides
Forced convection
Frequency ranges
Raman spectra
Tunable lasers
20-inch supersonic wind tunnel (SWT)
Air jets
Flow measurement
Flow visualization
Free flow
Freestream measurement
Hypersonic speed
Iodine
Laser induced fluorescence
Laser-induced thermal acoustics (LITA)
Mach number
Nonintrusive measurement
Rayleigh scattering
Supersonic combustion
Temperature
Turbulent jets
Velocity measurement
Wakes