Spectral intensity measurements from high-pressure nitrogen plasmas.
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Engineering topics
Publications and source records attributed to Cooper, D. M..
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Results are presented of an experimental program to measure the effect of radiative cooling on the enthalpy distribution behind incident shock waves traveling in air. The shock velocity was nominally 16 km/sec and the preshock ambient pressure was varied from 0.4 to 1.6 torr. Shock-tube diameters of 4.7 and 9.4 cm were used to investigate the effects of varying optical depths. Radiative cooling rates were determined from spatially resolved measurements of the profile of the H sub alpha line and from absolute measurements of the continuum radiation. The measured enthalpy profiles are in good agreement with the theoretical predictions of Chien and Compton which account for both nongrey and multidimensional aspects of the radiative transport in the shock tube.
Flow and radiative properties of air in high explosive shock tube
Radiative transport due to continua, molecular bands and atomic lines in inviscid nonadiabatic shock layer in stagnation region of blunt bodies
High resolution equilibrium radiation spectra for shock layer of blunt bodies at reentry velocities and radiative recombination of N and O ions
High resolution equilibrium radiation spectra for shock layer of blunt bodies at reentry velocities and radiative recombination of N and O ions
Free flight measurements of stagnation point convective heat transfer in air at hypersonic speeds
Free flight measurement of radiative heat load on circular cone and comparison with predicted equilibrium and nonequilibrium radiation
Measurement of aerodynamic heating on sharp cones entering earth atmosphere