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Design Charts of Static and Rotary Stability Derivatives for Cropped Double-delta Wings in Subsonic Compressible Flow

机译：亚音速可压缩流动双三角翼静，旋转稳定导数设计图

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作者
Lamar, J. E.;
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年度 1970
页码 1-8
总页数 8
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Aerodynamic configurations ; Delta wings ; Stability derivatives ; Structural design ; Subsonic flow ; Aircraft design ; Lifting bodies;

机译：空气动力学配置;三角翼;稳定性导数;结构设计;亚音速流动;飞机设计;升力体;
入库时间 2022-08-29 11:14:05

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1. Effect of thrust on the aeroelastic instability of a composite swept wing with two engines in subsonic compressible flow [J] . R. D. Firouz-Abadi, A. R. Askarian, P. Zarifian Journal of Fluids and Structures . 2013,第Null期

机译：推力对亚音速可压缩流中两引擎复合扫掠机翼气动弹性失稳的影响。
2. Robust aeroelastic instability suppression of an advanced wing with model uncertainty in subsonic compressible flow field [J] . Ji-Seok Song, Jeonghwan Choo, Seog-Ju Cha, Aerospace science and technology . 2013,第1期

机译：亚音速可压缩流场中具有模型不确定性的先进机翼的鲁棒气动弹性失稳抑制
3. Rapid computation of rotary derivatives for subsonic and low transonic flows [J] . Fu Jian-Ming, Tang Hai-Min, Chen Hong-Quan Engineering Computations . 2019,第9期

机译：亚音速和低跨音速流的旋转导数的快速计算
4. Investigation into the effects of juncture fillets on the vortical flow voer a cropped, double-delta wing [C] . Sheshagiri K. Hebbar, Max F. Platzer, Abdullah Al Khozam AIAA 32nd Aerospace Sciences Meeting Exhibit January 10-13, 1994/Reno, NV . -1

机译：研究接缝圆角对裁剪的双三角翼上旋涡流的影响
5. Unsteady compressible lifting surface analysis for rotary wings using velocity potential modes. [D] . Kaladi, Vasudevan Mundakizhi. 1990

机译：使用速度势模式对旋转机翼进行非稳态可压缩举升表面分析。
6. On the Existence of Subsonic Flows of a Compressible Fluid [O] . Max Shiffman 1952

机译：关于可压缩流体亚音速流的存在
7. Numerical studies of compressible flow over a double-delta wing at high angle of attack [O] . Coutley Raymond L. 1990

机译：高攻角下双三角翼可压缩流动的数值研究
8. Design charts of static and rotary stability derivatives for cropped double-delta wings in subsonic compressible flow [R] . Lamar, J. E. 1970

机译：亚音速可压缩流动中双三角翼的静态和旋转稳定性导数设计图

Design Charts of Static and Rotary Stability Derivatives for Cropped Double-delta Wings in Subsonic Compressible Flow

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