2016 · 11 citations · 6 references
EngineeringAerospace EngineeringAerodynamicsFluid DynamicsSensorsFlow MeasurementFlow MetrologyFlow SensorsHypersonic AerodynamicsShock WavesWind-tunnel TestingData ProcessingFlow Velocity MeasurementsHypersonic FlowLocal-field EffectsSchlieren ImagingTunable Laser DiodesVelocityVelocity Sensors
A new structure TDLAS velocity sensor for local hypersonic flow field and data processing method is presented. Schlieren images of the probe in wind tunnel tests show TDLAS measurement is barely influenced by shock layers.
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Tunable diode laser measurements on nitric oxide in a hypersonic wind tunnel
A. Mohamed, Bernard Rosier, D. Henry et al. · AIAA Journal · 1996 · 46 citations