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Effect of nose thickness distribution on the stall characteristics of low aspect ratio flying wing configuration at transonic flow

机译：鼻厚度分布对跨动力流动低纵横比飞行翼配置的失速特性的影响

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Xu ZHANG; JiXiang SHAN; Yong HUANG;
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1. Pitching effect on transonic wing stall of a blended flying wing with low aspect ratio [J] . Tao Yang, Zhao Zhongliang, Wu Junqiang, Modern Physics Letters, B. Condensed Matter Physics, Statistical Physics, Applied Physics . 2018,第12a13期

机译：用低纵横比对混合飞翼延长翼档的施放效果
2. Some compressibility effects on the lee side flow structures of cruciform wing-body configurations with very low aspect ratio wings [J] . S. Tilling, L. Dala, C. Toomer Aerospace science and technology . 2013,第1期

机译：纵横比非常低的十字形机翼构型的下风侧流动结构具有一定的压缩性
3. Lee-Side Flow Structures of Very Low Aspect Ratio Cruciform Wing-Body Configurations [J] . S. Tuling, L. Dala, C. Toomer Journal of Spacecraft and Rockets . 2013,第6期

机译：超低纵横比十字形机翼构型的Lee-Side流动结构
4. Aerodynamic shaping design and vortical flow design aspects of a 53deg swept flying wing configuration [C] . Andreas Schuette, Jan Vormweg, Ryan G. Maye, AIAA applied aerodynamics conference;AIAA aviation forum . 2018

机译：53度后掠翼配置的空气动力学造型设计和涡流设计方面
5. Dynamic Stall Characteristics of a Pitching Swept Finite Aspect Ratio Wing [D] . Tomek, Kristopher Ladd 2019

机译：俯仰扫掠有限长宽比机翼的动态失速特性
6. Characteristics of a simple high-resolution flow cytometer based o a new flow configuration. [O] . T Lindmo, H B Steen 1979

机译：基于新的流量配置的简单高分辨率流式细胞仪的特征。
7. Unsteady transonic flow calculations for wing-fuselage configurations [O] . Batina J. T. 1986

机译：机翼机身配置的非稳态跨音速流计算
8. The effects on the aerodynamic characteristics of varying the wing thickness ratio of a triangular wing-body configuration at transonic speeds from tests by the NACA wing-flow method [R] . Hall, Albert W, Mckay, James M 1952

机译：通过NaCa翼流法测试，在跨音速下改变三角翼体结构翼厚比的空气动力学特性

Effect of nose thickness distribution on the stall characteristics of low aspect ratio flying wing configuration at transonic flow

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