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Results of the orbiter wing and elevon load alleviation test in the NASA/MSFC 14-inch trisonic wind tunnel on a 0.004-scale model (74-OTS) Space Shuttle integrated vehicle (FA301)

机译：在0.004比例模型（74-OTs）航天飞机综合车辆（Fa301）上的Nasa / msFC 14英寸超音速风洞中的轨道器机翼和升降机负载减轻试验结果

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Poucher, D. E.;
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年度 1984
页码 1-635
总页数 635
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
CLIMBING FLIGHT; ELEVONS; LOADS (FORCES); SPACE SHUTTLE ASCENT STAGE; SPACE SHUTTLE ORBITERS; SPACECRAFT CONFIGURATIONS; SPACECRAFT DESIGN; SPACECRAFT STRUCTURES; STRUCTURAL DESIGN; WING PANELS; WINGS; AEROTHERMODYNAMICS; CONTROL SURFACES; DATA REDUCTION; DRAWINGS; EXTERNAL TANKS; FLOW DISTRIBUTION; GRAPHS (CHARTS); PLUMES; SCALE MODELS; SPACE SHUTTLE BOOSTERS; TABLES (DATA); TRANSONIC SPEED; TRISONIC WIND TUNNELS; WIND TUNNEL TESTS;

机译：攀登飞行;升降副翼;负荷（力量）;空间穿梭阶段; spaCE sHUTTLE ORBITERs;航天器配置;航天器设计;航天器结构;结构设计;翼板; WINGs;气动热力学;控制表面;数据减少;附图;外部坦克;流量分配;图表（图表）;羽毛;尺度模型; spaCE sHUTTLE BOOsTERs;表（数据）;跨音速; TRIsONIC WIND TUNNELs;风洞隧道测试;

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1. Gust load alleviation wind tunnel tests of a large-aspect-ratio flexible wing with piezoelectric control [J] . Bi Ying, Xie Changchuan, An Chao, 中国航空学报（英文版） . 2017,第001期

机译：压电控制大纵横比柔性机翼减轻风载荷的风洞试验
2. Wind-Tunnel Testing and Modeling of a Micro Air Vehicle with Flexible Wings [J] . R. Albertani, B. Stanford, R. DeLoach, Journal of Aircraft . 2008,第3期

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3. Passive gust alleviation of a flying-wing aircraft by analysis and wind-tunnel test of a scaled model in dynamic similarity [J] . He Shun, Guo Shijun, Liu Ying, Aerospace science and technology . 2021,第Juna期

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4. Aeroservoelastic Wind-Tunnel Tests of a Free-Flying, Joined-Wing SensorCraft Model for Gust Load Alleviation [C] . Robert C. Scott, Mark A. Castelluccio, David A. Coulson, AIAA/ASME/ASCE/AHS/ASC structures, structural dynamics and materials conference . 2011

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5. Aeroservoelastic Wind-Tunnel Tests of a Free-Flying, Joined-Wing SensorCraft Model for Gust Load Alleviation [O] . Castelluccio Mark A., Coulson David A., Heeg Jennifer, 2011

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6. Results of tests in the NASA/MSFC 14-inch trisonic wind tunnel on a 0.004-scale model (74-OTS) thrust augmented space shuttle integrated vehicle (IA602) [R] . Mansfield, A. C. 1983

机译：Nasa / msFC 14英寸超音速风洞在0.004比例模型（74-OTs）推力增强航天飞机综合车辆（Ia602）上的测试结果

Results of the orbiter wing and elevon load alleviation test in the NASA/MSFC 14-inch trisonic wind tunnel on a 0.004-scale model (74-OTS) Space Shuttle integrated vehicle (FA301)

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