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Supersonic Flow in the Area of Antisymmetric Thin Cruciform Wings with Supersonic Leading Edges in a Horizontal Plane, with Consideration of Flow Separation on the Edges.

机译：考虑边缘流动分离的水平面上超音速前缘反对称薄十字形翼区超声波流动。

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作者
Staicu, S.;
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年度 1978
页码 1-19
总页数 19
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Supersonic flow; Cruciform wings; Thin wings; Leading edges; Flow separation; Rumania; Translations;

机译：超音速流;十字形翅膀;薄翅膀;前缘;流动分离;罗马尼亚;翻译;

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专利

1. ESTIMATION OF SURFACE PRESSURE DISTRIBUTION ON A DELTA WING WITH CURVED LEADING EDGES IN HYPERSONIC/SUPERSONIC FLOW [J] . Asha Crasta, S. Pavitra, S. A. Khan International Journal of Energy, Environment and Economics . 2016,第1期

机译：超音速/超音速流动中具有弯曲前缘的三角翼表面压力分布的估计
2. SPECIAL SOLUTIONS FOR SUPERSONIC FLOW OF AN IDEAL GAS AROUND THE V-SHAPED WING WITH FLOW SEPARATIONS [J] . R. Ya. Tugazakov TsAGI science journal . 2015,第4期

机译：带流动分离的V形机翼周围理想气体超音速流动的特殊解决方案
3. Acoustic Leading-Edge Receptivity for Supersonic/Hypersonic Flows over a Blunt Wedge [J] . Cerminara Adriano, Sandham Neil D. AIAA Journal . 2017,第12期

机译：钝器上超音速/超人流的声学前沿接收
4. Calculation method for supersonic/hypersonic flows over configurations with blunt leading edges [C] . Dr.N.V.Voevodenko 1st AIAA Aircraft Engineering, Technology, and Operations Congress September 19-21, 1995/Los Angeles, CA . 1995

机译：超音速/超音速流动的计算方法，前缘钝化
5. High-resolution TVD schemes for the analysis of: I. Inviscid supersonic and transonic flows. II. Viscous flows with shock-induced separation and heat transfer. [D] . Driver, Mark Anthony. 1991

机译：用于分析以下内容的高分辨率TVD方案：I.超音速和跨音速无粘性流。二。粘性流具有激振引起的分离和热传递。
6. Investigations on the complex flows induced by dual-swept/dual-ramp wedges in supersonic flows [O] . X. Gao, G. X. Xiang, W. J. Tang, -1

机译：超音速流中双扫/双斜坡楔引起的复流研究
7. Calculation of supersonic viscous flow over delta wings with sharp subsonic leading edges [O] . Vigneron, Yvon Clovis 1978

机译：具有尖锐亚音速前缘的三角翼上超音速粘性流的计算
8. The Study of Supersonic Flow Around Delta Wings with Forced Antisymmetry Taking Into Consideration the Falling off of Flow at the Leading Edges. [R] . Staicu, S. 1978

机译：强迫反对称三角翼周围超音速流动的研究考虑了前缘流动的下降。

Supersonic Flow in the Area of Antisymmetric Thin Cruciform Wings with Supersonic Leading Edges in a Horizontal Plane, with Consideration of Flow Separation on the Edges.

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