抄録
A numerical method is developed for calculating a radiating axisymmetric flowfield accounting for nonequilibrium thermochemistry. Solutions of the flow with radiation are obtained in a fully coupled manner using a fully implicit time-marching method by the use of a full block matrix inversion. The method can be used in calculating both air and carbonaceous gas flows. Nonequilibrium radiation from a blunt body shock layer is calculated by the present method at a speed of up to 13.4 km/s. The calculated results are compared with existing experimental data. Fair agreement is obtained between the calculation and the experiment for the flight velocity below 10 km/s. For the case of 13.4 km/s, the calculated nonequilibrium radiative heat flux underestimates the measured value by a factor of 10.
本文言語 | English |
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出版ステータス | Published - 2000 12月 1 |
イベント | 38th Aerospace Sciences Meeting and Exhibit 2000 - Reno, NV, United States 継続期間: 2000 1月 10 → 2000 1月 13 |
Other
Other | 38th Aerospace Sciences Meeting and Exhibit 2000 |
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国/地域 | United States |
City | Reno, NV |
Period | 00/1/10 → 00/1/13 |
ASJC Scopus subject areas
- 宇宙惑星科学
- 航空宇宙工学