アーク放電型衝撃波管での輻射を伴うキセノンプラズマ流の実験
スポンサーリンク
概要
- 論文の詳細を見る
The electrical conductivity of xenon plasma in an arc driven shock tube was measured by means of a conductivity probe of magnetic induction type. The decay of continuous emission intensities was also measured at the two wavelengths 4425 Å and 3975Å. The initial xenon pressure (P<SUB>1</SUB>) ranged from 1.5 to 10 torr. The shock Mach number (M<SUB>s</SUB>) ranged roughly from 15 to 24. The effect of radiation cooling on the decay of electrical conductivity and that of continuous emission intensity was studied together with our previous measurements in a pressure driven shock tube, (P<SUB>1</SUB>= 1-5 torr and M<SUB>s</SUB> = 9-14).For higher. shock Mach numbers, the measured decrease of electrical conductivity and that of continuous emission intensity. could be correlated with continuum radiation loss. For lower shock Mach numbers at P<SUB>1</SUB>=1 and 2 torr, however, the decrease is much faster than the calculated value assuming continuum radiation loss alone. To obtain a possible explanation. for this discrepancy, the influence of line radiation loss was briefly discussed.
著者
関連論文
- 電極間電気抵抗の衝撃波管実験 : 核融合
- 7a-W-3 電離及び輻射を伴う衝撃波キセノン流れの研究
- 2a-K-3 衝撃波で加熱された希ガスの全電離緩和時間
- 11p-V-9 アルゴン衝撃波の電離緩和に及ぼす境界層の影響
- 19p-G-4 アーク放電型衝撃波管でのキセノンプラズマ流の実験
- 3p-GH-5 衝撃波プラズマのradiation cooling I
- アーク放電型衝撃波管での輻射を伴うキセノンプラズマ流の実験