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Theoretical calculations of the supersonic pressure distribution and wave drag for a limited family of tapered sweptback wings with symmetrical parabolic-arc sections at zero lift

机译：具有零升力对称抛物弧截面的有限锥形后掠翼系列的超音速压力分布和波阻的理论计算

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Kainer, Julian H;
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年度 1950
页码 1-16
总页数 16
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
WINGS, SWEPTBACK - TAPERED; DRAG, WAVE; PRESSURE DISTRIBUTION - WINGS, SWEPTBACK; AIRFOILS, CIRCULAR - ARC; AIRFOILS, SYMMETRICAL; THEORIES - WINGS SUPERSONIC;

机译：WINGs，sWEpTBaCK - TapERED; DRaG，WaVE;压力分布 - 翅膀，sWEpTBaCK;翼型，圆形 - 弧形;翼型，对称;理论 - WINGs sUpERsONIC;

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外文文献

1. Zero- Lift Wave Drag Calculation Using Supersonic Area Rule and Its Modifications [C] . V. Nikolic, E. Jumper AIAA Aerospace Sciences Meeting and Exhibit . 2004

机译：基于超音速面积法则的零升波阻力计算及其修正
2. THEORETICAL DETERMINATION OF THE PRESSURE DISTRIBUTION ON A LIFTING, SUBSONIC DELTA WING OF ARBITRARY ASPECT RATIO. [D] . SWAIN, CARL EUGENE. 1971

机译：从理论上确定任意纵横比的提升亚音速三角翼上的压力分布。
3. The theoretical wave drag at zero lift of fully-tapered swept wings of arbitrary section [O] . Nonweiler T. 1953

机译：任意截面的全锥形扫掠翼在零升程处的理论波浪阻力
4. Theoretical Calculations of the Supersonic Pressure Distribution and Wave Drag for a Limited Family of Tapered Sweptback Wings with Symmetrical Parabolic-Arc Sections at Zero Lift [R] . Kainer, J. H. 1950

机译：在零升程超音速压力分布和波阻圆锥后掠翼的有限家庭与对称抛物线弧段的理论计算

Theoretical calculations of the supersonic pressure distribution and wave drag for a limited family of tapered sweptback wings with symmetrical parabolic-arc sections at zero lift

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