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Cover image for Freestream Mach-number and temperature measurement in NASA Langley's 20-inch supersonic wind tunnel using laser-induced thermal acoustics

Freestream Mach-number and temperature measurement in NASA Langley's 20-inch supersonic wind tunnel using laser-induced thermal acoustics

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Cover image for Temperature and pressure dependence of signal amplitudes for electrostriction laser-induced thermal acoustics

Temperature and pressure dependence of signal amplitudes for electrostriction laser-induced thermal acoustics

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Cover image for Feasibility of Rayleigh scattering flow diagnostics in the National Transonic Facility

Feasibility of Rayleigh scattering flow diagnostics in the National Transonic Facility

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Cover image for Conical shock-strength determination on low-sonic-boom aircraft model by doppler global velocimetry

Conical shock-strength determination on low-sonic-boom aircraft model by doppler global velocimetry

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Cover image for Amplitude noise reduction of ion lasers with optical feedback

Amplitude noise reduction of ion lasers with optical feedback

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Cover image for Raman shifting a tunable ArF excimer laser to wavelengths of 190 to 240 nm with a forced convection Raman cell

Raman shifting a tunable ArF excimer laser to wavelengths of 190 to 240 nm with a forced convection Raman cell

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Cover image for Raman shifting a tunable ArF excimer laser to wavelengths of 190 to 240 nm with a forced convection Raman cell

Raman shifting a tunable ArF excimer laser to wavelengths of 190 to 240 nm with a forced convection Raman cell

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Joyner - Microforms B300 NAS 1.15:209710 ✔ Available
Cover image for Flow visualization by elastic light scattering in the boundary layer of a supersonic flow

Flow visualization by elastic light scattering in the boundary layer of a supersonic flow

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Joyner - Microforms B300 NAS 1.15:210121 ✔ Available