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Effects of wing elevation, incidence, and camber on the aerodynamic characteristics of a representative hypersonic cruise configuration at Mach numbers from 0.65 to 10.70

机译：机翼高度，入射和弯度对代表性高超音速巡航配置在马赫数为0.65到10.70时的空气动力学特性的影响

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摘要

Wing elevation, incidence, and chamber effects on aerodynamic characteristics of representative hypersonic cruise configuration at Mach numbers from 0.65 to 10.70

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作者
Axelson, J. A.; Nelms, W. P., Jr.;
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年度 1970
页码 1-77
总页数 77
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
AERODYNAMIC CHARACTERISTICS; AERODYNAMIC CONFIGURATIONS; FLIGHT TESTS; HYPERSONIC AIRCRAFT; AIRCRAFT STABILITY; CAMBERED WINGS; ELEVATION; HYPERSONIC SPEED; LIFT DRAG RATIO; PITCHING MOMENTS; WIND TUNNEL MODELS;

机译：空气动力学特征;空气动力学配置;飞行测试;超音速飞机;飞机稳定性; CamINGED WINGs;海拔;超速的;升降比; pITCHING mOmENTs;风洞模型;

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4. Aerodynamic performance and flow-field characteristics of two waverider-derived hypersonic cruise configurations [C] . Charles E. Cockrell, Lawrence D. Huebner, Dennis B. Finley AIAA 33rd Aerospace Sciences Meeting and Exhibit January 9-12, 1995/Reno, NV . -1

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5. Effects of spanwise camber on delta wing aerodynamics: An experimental and theoretical investigation. [D] . Traub, Lance Wayne. 1999

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6. Aerodynamic Performance and Flow-Field Characteristics of Two Waverider-Derived Hypersonic Cruise Configurations [O] . Huebner Lawrence D., Cockrell Charles E. Jr., Finley Dennis B. 1995

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Effects of wing elevation, incidence, and camber on the aerodynamic characteristics of a representative hypersonic cruise configuration at Mach numbers from 0.65 to 10.70

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