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Space shuttle: Static stability and control investigation of NR/GD delta wing booster (B-20) and delta wing orbiter (134-D), volume 3

机译：航天飞机：NR / GD三角翼助推器（B-20）和三角翼轨道器（134-D）的静态稳定性和控制研究，第3卷

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Experimental aerodynamic investigations have been made on a .0035 scale model North American Rockwell/General Dynamics version of the space shuttle in the NASA/MSFC 14 x 14 Inch Trisonic Wind Tunnel. Static stability and control data were obtained on the delta wing booster alone (B-20) and with the delta wing orbiter (134D) mounted in various positions on the booster. Six component aerodynamic force and moment data were recorded over an angle of attack range from -10 to 24 deg at 0 and 6 deg sideslip angles and from -10 to 10 deg sideslip at 0 deg angle of attack. Mach number ranged from 0.6 to 4.96.

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作者
Allen, E. C., Jr.; Eder, F. W.;
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年度 1972
页码 1-496
总页数 496
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
DELTA WINGS; SCALE MODELS; SPACE SHUTTLES; WIND TUNNEL STABILITY TESTS; AERODYNAMIC CHARACTERISTICS; ANGLE OF ATTACK; SPACE SHUTTLE BOOSTERS; SPACE SHUTTLE ORBITERS;

机译：DELTa WINGs;尺度模型;太空沙滩;风洞稳定性试验;空气动力学特征;攻击角度; spaCE sHUTTLE BOOsTERs; spaCE sHUTTLE ORBITERs;

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5. Static and dynamic leading-edge-flap effects on the vortex lift of a delta wing [D] . Karagounis, Thales 1997

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Space shuttle: Static stability and control investigation of NR/GD delta wing booster (B-20) and delta wing orbiter (134-D), volume 3

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