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Investigations on a 0.020-scale jet plume model (88-OTS) of the Rockwell International integrated SSV configuration 140C (modified) in the NASA/ARC 11-foot transonic wind tunnel (IA72), volume 4

机译：在Nasa / aRC 11英尺跨音速风洞（Ia72）中对罗克韦尔国际集成ssV配置140C（改进型）的0.020级喷射羽流模型（88-OTs）进行调查，第4卷

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Nichols, M. E.;
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年度 1977
页码 1-367
总页数 367
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
PLUMES; SPACE SHUTTLES; TRANSONIC WIND TUNNELS; WIND TUNNEL TESTS; BENDING MOMENTS; BODY-WING AND TAIL CONFIGURATIONS; SCALE MODELS; TRANSONIC SPEED;

机译：羽毛;太空沙滩;跨音风洞;风洞隧道测试;弯曲的时刻;身体和尾部的配置;尺度模型;跨音速;

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1. Comparison of the NASA Common Research Model European Transonic Wind Tunnel test data to NASA National Transonic Facility test data [J] . Melissa Rivers, Jürgen Quest, Ralf Rudnik CEAS Aeronautical Journal . 2018,第2期

机译：NASA通用研究模型欧洲跨音速风洞测试数据与NASA国家跨音速设施测试数据的比较
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机译：NASA兰利国家跨音速设施和NASA Ames 11-Ft跨音速风洞中的NASA通用研究模型的实验研究（邀请）
3. Experimental Investigations of the NASA Common Research Model in the NASA Langley National Transonic Facility and NASA Ames 11-Ft Transonic Wind Tunnel (Invited) [O] . Rivers S. M., Dittberner Ashley 2011

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4. Investigations on a 0.020-scale jet plume model (88-OTS) of the Rockwell International integrated SSV configuration 140C (modified) in the NASA/ARC 11-foot transonic wind tunnel (IA72), volume 5 [R] . Nichols, M. E. 1977

机译：对Nasa / aRC 11英尺跨音速风洞（Ia72）中Rockwell International集成ssV配置140C（改进型）的0.020级喷射羽流模型（88-OTs）的调查，第5卷

Investigations on a 0.020-scale jet plume model (88-OTS) of the Rockwell International integrated SSV configuration 140C (modified) in the NASA/ARC 11-foot transonic wind tunnel (IA72), volume 4

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