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Pressure test of several models in air-carbon- dioxide mixtures in the 21-inch hypersonic wind tunnel

机译：在21英寸高超声速风洞中的几种模型在空气 - 二氧化碳混合物中的压力测试

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Hypersonic wind tunnel tests of models in air-carbon dioxide mixtures

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作者
Blaylock, R. B.;
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年度 1964
页码 1-12
总页数 12
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
CARBON DIOXIDE; DIOXIDES; HYPERSONIC WIND TUNNELS; WIND TUNNEL TESTS; CARBON DIOXIDE; HYPERSONIC WIND TUNNEL;

机译：二氧化碳;二氧化物;超级风洞;风洞隧道测试;二氧化碳; HYpERsONIC WIND TUNNEL;

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2. Accurate attitude estimation of HB2 standardmodel based on QNCF in hypersonic wind tunnel test [J] . Haotian YANG, Bin ZHOU, Qi WEI, 中国航空学报（英文版） . 2020,第001期

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机译：基于单矢量系统的风洞力平衡的热压特性实验设计与分析方法，用于高超声速风洞研究中的压力和温度效应模型
5. Pressure distribution on the roof of a model low-rise building tested in a boundary layer wind tunnel. [D] . Goliber, Matthew Robert. 2009

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6. Wind Tunnel Tests for Wind Pressure Distribution on Gable Roof Buildings [O] . Xiao-kun Jing, Yuan-qi Li 2013

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7. Pressure distribution on the roof of a model low-rise building tested in a boundary layer wind tunnel [O] . Goliber, Matthew Robert 2009

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8. Data Report of JPL wind tunnel tests of a 0.030-scale Apollo dynamic stability model (FD-1) in the 20-inch supersonic (test no. 20-516) and the 21-inch hypersonic (test no. 21-113) tunnels [R] . 1963

机译：在20英寸超音速（测试号20-516）和21英寸高超音速（测试号21-113）隧道中的0.030比例apollo动态稳定性模型（FD-1）的JpL风洞试验数据报告

Pressure test of several models in air-carbon- dioxide mixtures in the 21-inch hypersonic wind tunnel

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