CO concentration and gas temperature distribution are diagnosed behind a strong shock wave simulating the Martian atmosphere entry processes by coupling optical emission spectroscopy (OES) and tunable diode laser absorption spectroscopy (TDLAS). The strong shock wave (6.31 +/- A 0.11 km/s) is established in a shock tube driven by combustion of hydrogen and oxygen. Temperature of the shock-heated gas is inferred through a precise analysis of the high temporal and spatial resolution experimental spectral of CN violet system (B (2) I pound (+) -> X (2) I pound (+), Delta v = 0 sequence) using OES. A CO absorption line near 2,335.778 nm is utilized for detecting the CO concentration using scanned-wavelength direct absorption mode with 50 kHz re...
This work represents efforts to study high-enthalpy carbon dioxide flows in anticipation of the upc...
Effects of water vapor presence in Martian atmospheric entry plasma (MAEP) were calculated based on ...
Thermochemical relaxation behind a normal shock in Mars and Titan gas mixtures is simulated using a ...
Shock tube experiments are carried out to study the physical and chemical processes during a vehicle...
Predicting and managing heat transfer during planetary entry is a critical engineering challenge for...
Incident shock waves in pure CO have been characterized in the Electric Arc ShockTube facility at NA...
The mechanism of CO2 dissociation during entry in the Mars atmosphere is experimentally investigated...
Non-equilibrium radiation measurements behind strong shock wave for simulated Martian atmosphere are...
This work represents ongoing efforts to study high-enthalpy carbon dioxide flows in anticipation of ...
This paper reports on the measurement of radiative heating for shock heated flows which simulate con...
Estimate of chemical kinetics behind normal shock waves in carbon dioxide and nitrogen mixtures for ...
This paper represents a summary of results to date of an on-going effort at NASA Ames Research Cente...
This thesis investigates the modelling of radiating shock layers encountered during atmospheric entr...
The shock standoff distance in front of a blunt body is sensitive to the thermochemical state of th...
International audienceNonequilibrium infrared emission spectra representative of a Mars atmospheric ...
This work represents efforts to study high-enthalpy carbon dioxide flows in anticipation of the upc...
Effects of water vapor presence in Martian atmospheric entry plasma (MAEP) were calculated based on ...
Thermochemical relaxation behind a normal shock in Mars and Titan gas mixtures is simulated using a ...
Shock tube experiments are carried out to study the physical and chemical processes during a vehicle...
Predicting and managing heat transfer during planetary entry is a critical engineering challenge for...
Incident shock waves in pure CO have been characterized in the Electric Arc ShockTube facility at NA...
The mechanism of CO2 dissociation during entry in the Mars atmosphere is experimentally investigated...
Non-equilibrium radiation measurements behind strong shock wave for simulated Martian atmosphere are...
This work represents ongoing efforts to study high-enthalpy carbon dioxide flows in anticipation of ...
This paper reports on the measurement of radiative heating for shock heated flows which simulate con...
Estimate of chemical kinetics behind normal shock waves in carbon dioxide and nitrogen mixtures for ...
This paper represents a summary of results to date of an on-going effort at NASA Ames Research Cente...
This thesis investigates the modelling of radiating shock layers encountered during atmospheric entr...
The shock standoff distance in front of a blunt body is sensitive to the thermochemical state of th...
International audienceNonequilibrium infrared emission spectra representative of a Mars atmospheric ...
This work represents efforts to study high-enthalpy carbon dioxide flows in anticipation of the upc...
Effects of water vapor presence in Martian atmospheric entry plasma (MAEP) were calculated based on ...
Thermochemical relaxation behind a normal shock in Mars and Titan gas mixtures is simulated using a ...