Computational Assessment of a 3-Stage Axial Compressor Which Provides Airflow to the NASA 11- by 11-Foot Transonic Wind Tunnel, Including Design Changes for Increased Performance.

著录项

• 作者

  Kulkarni, S.; Beach, T. A.; Jorgenson, P. C.; Veres, J. P.;

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• 作者单位

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• 年度 2017
• 页码 1-10
• 总页数 10
• 原文格式 PDF
• 正文语种 eng
• 中图分类
• 关键词

  Computational fluid dynamics; Aerodynamic characteristics; Aluminum alloys; Design analysis; Transonic wind tunnels; Turbomachinery; Turbocompressors; Pressure ratio; Boundary conditions; Compressors; Performance prediction; Test chambers;

  机译：计算流体动力学;空气动力学特性;铝合金;设计分析;跨音速风洞;涡轮机械;涡轮压缩机;压力比;边界条件;压缩机;性能预测;试验箱;
• 入库时间 2022-08-29 10:46:29