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Real-Helium Hypersonic Flow Parameters for Pressures to 3600 Atmospheres and Temperatures to 15,000 Deg K

机译：真氦高超声速流动参数压力为3600大气压，温度为15,000摄氏度

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作者
Miller, C. G.; Wilder, S. E.;
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年度 1968
页码 1-4
总页数 4
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Equations of state ; Hotshot wind tunnels ; Hypersonic flow ; Parameterization ; Free flow ; Helium ; High temperature fluids ; Normal shock waves ; Nozzle flow;

机译：状态方程; Hotshot风洞;高超声速流;参数化;自由流动;氦;高温流体;正常冲击波;喷嘴流;

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1. Recent advances in the application of discharge-flow to the determination of gas-phase rate coefficients at pressures and temperatures of relevance to the Earth's atmosphere [J] . Percival CJ, Shallcross DE, Canosa-Mas CE, Journal of Photochemistry and Photobiology, A. Chemistry . 2005,第1a3期

机译：在确定与地球大气有关的压力和温度下的气相流量系数的应用中，排放流的最新进展
2. Measurements of parameters of transient gas flows by a diode laser absorption spectroscopy at elevated pressures and temperatures [J] . Bolshov M. A., Kuritsyn Yu. A., Liger V. V., Optics and Spectroscopy . 2017,第5期

机译：电压和温度下二极管激光吸收光谱法测量瞬态气体流量的测量
3. Viscosities, nissan parameter and activation energies of viscous flow of N,N-dimethyl formamide and methanol at 25 deg C, 30 deg and 35 deg C [J] . Y. P. Singh, A. Prakash, Anju Bala Singh Oriental Journal of Chemistry: An International Research Journal of Pure & Applied Chemistry . 2003,第1期

机译：N，N-二甲基甲酰胺和甲醇在25°C，30°C和35°C的粘度，粘度，日产参数和活化能
4. Temperature- Cancelled Anodized- Aluminum Pressure Sensitive Paint for Hypersonic Compression Corner Flows [C] . T. Kuriki, H. Sakaue, O. Imamura, AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition . 2010

机译：用于超音速压缩角流的温度消除阳极氧化铝压敏涂料
5. Amino acids under hydrothermal conditions: Apparent molar volumes, apparent molar heat capacities, and acid /base dissociation constants for aqueous alpha-alanine, beta-alanine, glycine, and proline at temperatures from 25 to 250°C and pressures up to 30.0 MPa. [D] . Clarke, Rodney George Francis. 2000

机译：水热条件下的氨基酸：在25至250°C的温度和最高30.0 MPa的压力下，水性α-丙氨酸，β-丙氨酸，甘氨酸和脯氨酸的表观摩尔体积，表观摩尔热容量和酸/碱解离常数。
6. Thermodynamic Properties of Fluid Oxygen at Temperatures to 250 K and Pressures to 350 Atmospheres on Isochores at 1.3 to 3.0 Times Critical Density [O] . Robert D. Goodwin 1969

机译：在等压线上温度为250 K压力为350大气压力下流体氧的热力学性质为临界密度的1.3到3.0倍
7. Molecule-based approach for computing chemical-reaction rates in upper atmosphere hypersonic flows. [O] . Gallis, Michail A., Bond, Ryan Bomar, Torczynski, John Robert 2009

机译：基于分子的方法计算高层大气超音速流动中的化学反应速率。
8. Real-helium hypersonic flow parameters for pressures to 3600 atmospheres and temperatures to 15,000 deg K [R] . Miller, C. G., III, Wilder, S. E. 1968

机译：真氦高超声速流动参数，压力为3600个大气压，温度为15,000度K

Real-Helium Hypersonic Flow Parameters for Pressures to 3600 Atmospheres and Temperatures to 15,000 Deg K

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