Calculation of radiating flowfield behind a reflected shock wave in air

Takeharu Sakai; Keisuke Sawada; Chul Park

doi:10.2514/6.1998-861

Calculation of radiating flowfield behind a reflected shock wave in air

Takeharu Sakai, Keisuke Sawada, Chul Park

ENG - Aerospace Engineering

Research output: Contribution to conference › Paper › peer-review

Abstract

A numerical method for calculating a one-dimensional radiating flowfield in thermochemical equilibrium in which radiation strongly affects the flowfield is developed. Radiative heat fluxes are calculated using a model developed earlier which combines Planck, Rosseland and Gray-gas models. The flow solution is obtained with a fully implicit time-marching method using a full block matrix inversion. The method is applied for calculating a radiating flowfield behind a reflected shock wave in air. It is shown that (1) the method converges at enthalpies up to 100 MJ/kg and pressure up to 5 atm, and that (2) the calculated radiative heat flux values agree fairly well with the experimental data taken at enthalpies of up to 80 MJ/kg.

Original language	English
DOIs	https://doi.org/10.2514/6.1998-861
Publication status	Published - 1998
Event	36th AIAA Aerospace Sciences Meeting and Exhibit, 1998 - Reno, United States Duration: 1998 Jan 12 → 1998 Jan 15

Other

Other	36th AIAA Aerospace Sciences Meeting and Exhibit, 1998
Country	United States
City	Reno
Period	98/1/12 → 98/1/15

ASJC Scopus subject areas

Engineering(all)
Space and Planetary Science

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abstract = "A numerical method for calculating a one-dimensional radiating flowfield in thermochemical equilibrium in which radiation strongly affects the flowfield is developed. Radiative heat fluxes are calculated using a model developed earlier which combines Planck, Rosseland and Gray-gas models. The flow solution is obtained with a fully implicit time-marching method using a full block matrix inversion. The method is applied for calculating a radiating flowfield behind a reflected shock wave in air. It is shown that (1) the method converges at enthalpies up to 100 MJ/kg and pressure up to 5 atm, and that (2) the calculated radiative heat flux values agree fairly well with the experimental data taken at enthalpies of up to 80 MJ/kg.",

author = "Takeharu Sakai and Keisuke Sawada and Chul Park",

note = "Publisher Copyright: {\textcopyright} 1998 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved. Copyright: Copyright 2020 Elsevier B.V., All rights reserved.; 36th AIAA Aerospace Sciences Meeting and Exhibit, 1998 ; Conference date: 12-01-1998 Through 15-01-1998",

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AU - Sakai, Takeharu

AU - Sawada, Keisuke

AU - Park, Chul

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N2 - A numerical method for calculating a one-dimensional radiating flowfield in thermochemical equilibrium in which radiation strongly affects the flowfield is developed. Radiative heat fluxes are calculated using a model developed earlier which combines Planck, Rosseland and Gray-gas models. The flow solution is obtained with a fully implicit time-marching method using a full block matrix inversion. The method is applied for calculating a radiating flowfield behind a reflected shock wave in air. It is shown that (1) the method converges at enthalpies up to 100 MJ/kg and pressure up to 5 atm, and that (2) the calculated radiative heat flux values agree fairly well with the experimental data taken at enthalpies of up to 80 MJ/kg.

AB - A numerical method for calculating a one-dimensional radiating flowfield in thermochemical equilibrium in which radiation strongly affects the flowfield is developed. Radiative heat fluxes are calculated using a model developed earlier which combines Planck, Rosseland and Gray-gas models. The flow solution is obtained with a fully implicit time-marching method using a full block matrix inversion. The method is applied for calculating a radiating flowfield behind a reflected shock wave in air. It is shown that (1) the method converges at enthalpies up to 100 MJ/kg and pressure up to 5 atm, and that (2) the calculated radiative heat flux values agree fairly well with the experimental data taken at enthalpies of up to 80 MJ/kg.

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T2 - 36th AIAA Aerospace Sciences Meeting and Exhibit, 1998

Y2 - 12 January 1998 through 15 January 1998

ER -

Calculation of radiating flowfield behind a reflected shock wave in air

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