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Airloads investigation of an 0.030 scale model of the space shuttle vehicle 140A/B orbiter configuration (model 47-0) in the arc 9 by 7-foot unitary plan wind tunnel for Mach 1.55 and 2.2 (OA22B)

机译：空中载荷调查航天飞机车辆140a / B轨道飞行器配置（型号47-0）的0.030比例模型，用于马力1.55和2.2（Oa22B）的7英尺单一平面风洞的弧形9

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For abstract, see N75-23647.

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Gillins, R. L.;
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年度 1975
页码 1-762
总页数 762
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
LAUNCH VEHICLE CONFIGURATIONS; SPACE SHUTTLE ORBITERS; WIND TUNNEL MODELS; WIND TUNNEL TESTS; AERODYNAMIC LOADS; ANGLE OF ATTACK; PRESSURE DISTRIBUTION; SIDESLIP; SPACE SHUTTLE BOOSTERS; SUPERSONIC SPEED; WING TANKS;

机译：发射车辆配置; spaCE sHUTTLE ORBITERs;风洞模型;风洞隧道测试;空气动力负荷;攻击角度;压力分布;侧滑; spaCE sHUTTLE BOOsTERs;超音速; WING TaNKs;

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5. Flow-field measurements in the windward surface shock layer of space shuttle orbiter configurations at Mach number 8 [O] . Carter, L. D., Martindale, W. R. 1975

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Airloads investigation of an 0.030 scale model of the space shuttle vehicle 140A/B orbiter configuration (model 47-0) in the arc 9 by 7-foot unitary plan wind tunnel for Mach 1.55 and 2.2 (OA22B)

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