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Data report for static pressure tests of the Apollo PSTL-1 model in NAA Trisonic Wind Tunnel /TWT 77/, volume 1

机译：Naa Trisonic Wind Tunnel / TWT 77 /，第1卷apollo psTL-1型静压试验数据报告

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年度 1962
页码 1-523
总页数 523
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
APOLLO SPACECRAFT; PRESSURE DISTRIBUTION; WIND TUNNEL STABILITY TESTS; RESEARCH PROJECTS; SPACECRAFT CONFIGURATIONS; STATIC PRESSURE;

机译：apOLLO spaCECRaFT;压力分布;风洞稳定性试验;研究项目;航天器配置;静压力;

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3. Comparison of Static Aerodynamic Data Obtained in Dynamic Wind Tunnel Tests and Numerical Simulation Research [J] . Belaidouni Habib, Samard?i? Marija ?., Jerkovi? Damir D., Technical Gazette . 2018,第2期

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5. Uncertainty Analysis of Test Data at the NRC 1.5 Meter Trisonic Wind Tunnel = [D] . Fakhraei, Samin. 2016

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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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8. Data report for tests of a 0.105 scale Apollo /FS-2/ static force model to evaluate various post-abort configurations at Mach numbers 0.4 to 3.5 in the NAA Trisonic Wind Tunnel /TWT-90/ [R] . Cummings, D. G., Mitchell, C. 1963

机译：用于测试0.15比例apollo / Fs-2 /静力模型的数据报告，以评估Naa Trisonic风洞/ TWT-90 /中马赫数为0.4至3.5的各种中止后配置

Data report for static pressure tests of the Apollo PSTL-1 model in NAA Trisonic Wind Tunnel /TWT 77/, volume 1

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