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Part I. Experimental investigation of an arc-heated supersonic free jet. Part II. Analysis of one-dimensional isentropic flow for partially ionized argon

机译:第一部分。电弧加热超音速自由射流的实验研究。第二部分。部分电离氩的一维等熵流分析

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摘要

NOTE: Text or symbols not renderable in plain ASCII are indicated by [...]. Abstract is included in .pdf document.I. Experimental Investigation of an Arc-Heated Supersonic Free Jet.An experimental investigation of the flow field of a highly ionized supersonic free jet has been carried out in a continuous-flow test facility. Measurements of impact pressure, mass flux, total enthalpy and stagnation point heat transfer profile were made in this flow field with two water cooled probes.Argon gas, at a flowrate of 0.5 gm/sec, was heated in a magneto-plasma-dynamic arc heater without an external magnetic field operating from between 200 amp and 40 volts to 1000 amp and 25 volts. The total pressure ranged from between 20 and 35 mm Hg, at constant flowrate, and the atom-ion number density was approximately [...] cm[...] at the exit plane. The average total enthalpy calculated from a heat balance ranged from between about 5,000 to 10,000 BTU/[...], while the probe measurements showed that the peak total enthalpy on the jet centerline near the exit plane was about three times the average total enthalpy.The impact and mass flux measurements showed that the flow was hypersonic, source-like, chemically frozen, and in other details very much like the under-expanded free jet flow of a perfect gas. By combining these measurements with the total enthalpy measurements it was shown that the fraction of the total energy contained in ionization was about 0.6 which is quite close to the equilibrium stagnation value. For equilibrium stagnation conditions, the total temperature ranges from between 12,000° to 20,000°K. The species mass fraction ranges from 0.2 for the atoms and 0.8 for the singly-ionized ions, to 0.8 for the singly-ionized ions and 0.2 for doubly-ionized ions.Examination of the electron energy equation showed that within a few diameters from the exit plane the electrons become energetically isolated from the ions and the electron heat conduction term dominates.A preliminary attempt to correlate the stagnation point heat transfer measurements along the axis shows that the electron temperature (TE [...] TI in general) plays an important role.II. Analysis of One-Dimensional Isentropic Flow for Partially Ionized Argon.One-dimensional isentropic-flow variables of partially ionized argon have been calculated by coupling the isentropic flow equations with the partition-function method of deriving equilibrium thermodynamic properties. Tabulated gas properties and flow variables are presented for stagnation conditions of 0.1, 0.5, 1.0, 2.0, and 3.0 atm pressure and temperatures from 6,000 to 14,000°K in 1,000°K increments. The gas properties computed for this flow process include the sound speed, entropy, enthalpy, electron concentration, ionization fraction, electrical conductivity and static-to-stagnation ratios of temperature, pressure, and density. Flow variables include velocity, mass flux, area ratio, and Reynolds number per centimeter. Compared to results obtainable from perfect gas relationships (neglecting excitation and ionization), the results indicate that electronic excitation, and especially ionization effects, significantly alter the flow variables, particularly at the lower stagnation pressures and higher temperatures considered. However, with the exception of the effect of one excited state (the first excited state of the ion) on the equilibrium-composition equation, the thermodynamic properties calculated by neglecting excitation yielded results which were within 1% of those predicted by including excitation.
机译:注意:用[...]表示无法用纯ASCII呈现的文本或符号。摘要包含在.pdf文件中。电弧加热的超音速自由射流的实验研究在连续流动测试设备中对高电离的超音速自由射流的流场进行了实验研究。用两个水冷探头在该流场中测量冲击压力,质量通量,总焓和停滞点传热曲线。在磁等离子体动力电弧中加热流量为0.5 gm / sec的氩气加热器没有200伏至40伏至1000伏至25伏之间的外部磁场。固定流速下的总压力范围为20毫米汞柱至35毫米汞柱,出口平面处的原子离子数密度约为cm cm。根据热平衡计算出的平均总焓在大约5,000至10,000 BTU / [...]之间,而探针测量表明,出口平面附近射流中心线上的总总焓约为平均总焓的三倍冲击和质量通量测量表明,该流是超音速的,类似源的,化学冻结的,在其他细节上非常类似于理想气体的膨胀不足的自由射流。通过将这些测量值与总焓值测量值相结合,可以看出电离中所含总能量的比例约为0.6,这非常接近于平衡停滞值。对于平衡停滞条件,总温度范围为12,000°至20,000°K。物质的质量分数范围从原子的0.2,单电离的离子0.8到单电离的离子0.8以及双电离的离子0.2。对电子能量方程的研究表明,在出口的几个直径范围内电子与离子在能量平面上隔离开来,并且电子导热项占主导地位。初步尝试将沿轴向的停滞点传热测量结果相关联,表明电子温度(通常为TE TI)起着重要的作用。角色部分离子化氩的一维等熵流分析。通过将等熵流方程与分配函数相结合,得出平衡热力学性质,计算了部分离子化氩的一维等熵流变量。表中列出了在0.1、0.5、1.0、2.0和3.0大气压的停滞条件以及6,000至14,000°K的温度(以1,000°K为增量)下的制表气体特性和流量变量。为该流动过程计算的气体性质包括声速,熵,焓,电子浓度,电离分数,电导率以及温度,压力和密度的静滞比。流量变量包括速度,质量通量,面积比和每厘米雷诺数。与从完美的气体关系(忽略激发和电离)获得的结果相比,结果表明,电子激发,尤其是电离效应,显着改变了流量变量,特别是在较低的停滞压力和较高的温度下。但是,除了一个激发态(离子的第一个激发态)对平衡组成方程的影响外,忽略激发计算出的热力学性质所得出的结果与包含激发所预测的结果相差1%之内。

著录项

  • 作者

    Witte Arvel Benjamin;

  • 作者单位
  • 年度 1967
  • 总页数
  • 原文格式 PDF
  • 正文语种 {"code":"en","name":"English","id":9}
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