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Results of an investigation of aerodynamic forces, moments, and pressures on 0.03-scale models of the mated space shuttle orbiter and carrier aircraft (model nos.47.0 and AX1319P-1) in the Boeing transonic wind tunnel (CA9), volume 3

机译：波音跨音速风洞（Ca9）中配对的航天飞机轨道飞行器和运载机（型号编号47.0和aX1319p-1）的0.03比例模型的空气动力，力矩和压力调查结果，第3卷

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Hersey, D. W.;
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年度 1979
页码 1-964
总页数 964
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
AERODYNAMIC CHARACTERISTICS; BOEING 747 AIRCRAFT; SPACE SHUTTLE ORBITERS; TRANSONIC WIND TUNNELS; WIND TUNNEL TESTS; MOMENT DISTRIBUTION; PRESSURE DISTRIBUTION; TABLES (DATA); TORQUE; TRANSONIC SPEED;

机译：空气动力学特征;波音747飞机; spaCE sHUTTLE ORBITERs;跨音风洞;风洞隧道测试;时间分配;压力分布;表（数据）;扭矩;跨音速;

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6. Results of an investigation of aerodynamic forces, moments, and pressures on 0.03-scale models of the mated space shuttle orbiter and carrier aircraft (model nos.47-0 and AX1319P-1) in the Boeing transonic wind tunnel (CA9), volume 4 [R] . Hersey, D. W. 1979

机译：波音跨音速风洞（Ca9）中配对的航天飞机轨道飞行器和运载机（型号编号47-0和aX1319p-1）的0.03比例模型的空气动力，力矩和压力调查结果，第4卷

Results of an investigation of aerodynamic forces, moments, and pressures on 0.03-scale models of the mated space shuttle orbiter and carrier aircraft (model nos.47.0 and AX1319P-1) in the Boeing transonic wind tunnel (CA9), volume 3

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