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NF-6增压连续式跨声速风洞流场特性与标模试验 被引量:6

The test of characteristics of flow area and calibration model in NF-6 pressurized continuous transonic wind tunnel
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摘要 NF-6风洞是中国第一座增压连续式跨声速风洞。对NF-6风洞试验段流场特性进行了总结分析,研究结果表明该风洞具有优良的流场品质,总体上达到了设计要求,具备了承担型号和科研试验任务的能力。通过AGARD-B标模试验,进一步完善了NF-6风洞试验段流场品质校测项目,检验了该风洞的测力试验能力。NF-6风洞标模试验结果与国内外风洞试验数据吻合较好,试验精度和风洞平均气流偏角满足国军标要求,表明该风洞具备了测力试验的能力。 NF-6 wind tunnel is the first pressurized continuous transonic wind tunnel in Chi- na. The characteristics of flow area of test section in NF-6 wind tunnel were summarized and ana- lyzed. The study results indicate that this wind tunnel possesses nicer quality of flow area and the design request is achieved. Consequently, the NF-6 wind tunnel has the ability of conducting model and scientific research test. In order to validate the quality of flow area and test ability of NF-6 wind tunnel, the force test of AGARD-B calibration model was conducted. The test results coincide with the data of other wind tunnels and the test precision and average flow skew angle both satisfy the requirement of GJB. It shows that NF-6 wind tunnel has the ability of conducting force test.
出处 《实验流体力学》 CAS CSCD 北大核心 2013年第1期61-64,92,共5页 Journal of Experiments in Fluid Mechanics
基金 国家863计划资助项目(863-2007AA11Z243) 西北工业大学基础研究基金(JC-201103)
关键词 跨声速风洞 连续式 试验段 流场特性 标模试验 transonic wind tunnel continuous test section characteristics of flow area cali-bration model test
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参考文献4

  • 1乔志德.西工大NF6增压连续式高速翼型风洞论证报告[R].NF-6风洞设计方案评审会资料,1997.
  • 2范洁川.风洞实验手册[M].北京:航空工业出版社.2002.
  • 3恽起麟.高速风洞和低速风洞流场品质规范[s].GJBll79-1991,1991.
  • 4恽起麟.高速风洞和低速风洞测力实验精度指标[S].GJB]061-1991,1991.

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