1994
DOI: 10.2514/3.525
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Compatibility of infrared band models with scattering

Abstract: Techniques for the computation of radiative heating from aluminized solid propellant rocket exhaust plumes must account for infrared emission and absorption by hot H 2 O and CO 2 in the presence of strong threedimensional aerosol scattering by micron-sized A1 2 O 3 droplets and particles. Radiative heating computations are usually performed over wide spectral intervals using infrared band models. However, no rigorous extension to infrared band models has been proposed for situations with scattering. Indeed, ba… Show more

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Cited by 5 publications
(7 citation statements)
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“…(14), was conducted rst without iteration. Once the nonscattered part was obtained, the scattered part was calculated with terms containing N I nm acting as known source terms.…”
Section: Resultsmentioning
confidence: 99%
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“…(14), was conducted rst without iteration. Once the nonscattered part was obtained, the scattered part was calculated with terms containing N I nm acting as known source terms.…”
Section: Resultsmentioning
confidence: 99%
“…The transfer equation for nonscattered radiation, Eq. (14), was solved using the ray-tracingmethod described by Liu. 7 Ray tracing was performed at the center of each computational grid along all the directions de ned by the T 4 quadrature set (128 directions).…”
Section: Resultsmentioning
confidence: 99%
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