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handbook of infrared radiation from combustion gasesThe 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.
Document ID
19730019075
Document Type
Special Publication (SP)
Authors
Ludwig, C. B.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Malkmus, W.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Reardon, J. E.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Thomson, J. A. L.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Goulard, R.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1973
Subject Category
THERMODYNAMICS AND COMBUSTION
Report/Patent Number
NASA-SP-3080
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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