A Study of the Influence of Carbon Dioxide on Infrared Radiative Transfer in the Stratosphere and Mesosphere
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Spectral composition of earth radiation determined using monochromators installed on board Cosmos series earth satellites
Volume backscattering functions and optical extinction coefficients for visible and IR RADIATION and selected cloud models
Appleton-Hartree equations for propagation of electromagnetic waves collisionless magnetoionic medium to determine effect of electron density on laser behavior
IR radiation heat transfer from rocket exhaust plumes, discussing absorption and emission characteristics
Absorption of black-body radiation by ice cryodeposits on metal substrates
IR spectral distribution from region between stars of Trapezium in Orion Nebula
Residual interstellar gas from protostar formation detected as high luminosity IR object
IR radiation intensity distribution in solar neighborhood from grain models of dirty ice, graphite and graphite core-dirty ice mantle
Cosmic IR radiation sources, discussing galactic and stellar masses
Rocket observations of far IR radiation from upper atmosphere
Simultaneous meteorological satellite IR radiation measurements and cloud photographs for superposition and mutual interpretation
Four-color IR photometry of cool carbon, S and M stars
IR radiation role in limiting central heater maximum temperature and heat transfer to high density oxygen in cryogenic storage systems
Lunar IR directional characteristics theory, noting agreement with observations at all observational and phase angles
The absorption coefficients of 1.15- and 3.39-micrometer radiation for a homogeneous H-He plasma have been measured in a temperature and electron density range where the major absorption mechanisms are electron-ion inverse bremsstrahlung and neutral-atom photoionization. Measurements were made behind both the incident and reflected shock waves in a driven tube by recording the laser intensity transmitted along the tube diameter as a function of time. The measured values compare well with those obtained from theoretical calculations for a gas in thermodynamic equilibrium.
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The treatment of radiant emission and absorption by combustion gases are discussed. Typical applications include: (1) rocket combustion chambers and exhausts, (2) turbojet engines and exhausts, and (3) industrial furnaces. Some mention is made of radiant heat transfer problems in planetary atmospheres, in stellar atmospheres, and in reentry plasmas. Particular consideration is given to the temperature range from 500K to 3000K and the pressure range from 0.001 atmosphere to 30 atmospheres. Strong emphasis is given to the combustion products of hydrocarbon fuels with oxygen, specifically to carbon dioxide, water vapor, and carbon monoxide. In addition, species such as HF, HC1, CN, OH, and NO are treated.