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An engineering method for modeling the interaction of circular bodies and very low aspect ratio cruciform wings at supersonic speeds

机译：一种在超音速下模拟圆形体与极低纵横比十字形翼的相互作用的工程方法

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Tuling S;
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1. 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
2. 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
3. Aerodynamic Characteristics of a Low Aspect Ratio Wing and Propeller Interaction for a Tilt-Body MAV [J] . Kwanchai Chinwicharnam, David Gomez Ariza, Jean-Marc Moschetta, International journal of micro air vehicles . 2013,第4期

机译：车身倾斜的低纵横比机翼和螺旋桨相互作用的空气动力学特性
4. An Engineering Method for Very Low Aspect Ratio Cruciform Wing-Body Configurations [C] . S. Tilling, L. Dala, C. Toomer AIAA applied aerodynamics conference . 2013

机译：极低纵横比十字形机翼构型的工程方法
5. Investigation of low blowing ratio blended missile body supersonic jet interaction flowfields. [D] . Mahmud, Zakaria. 2003

机译：低吹速混合弹体超音速射流相互作用流场的研究。
6. A vortex model for forces and moments on low-aspect-ratio wings in side-slip with experimental validation [O] . Adam C. DeVoria, Kamran Mohseni -1

机译：侧滑低纵横比机翼上力和力矩的涡流模型并通过实验验证
7. An engineering method for modeling the interaction of circular bodies and very low aspect ratio cruciform wings at supersonic speeds [O] . Tuling S. 100

机译：一种在超音速下模拟圆形体与极低纵横比十字形翼的相互作用的工程方法
8. Lift, drag, and pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds : an investigation at large Reynolds numbers of the low-speed characteristics of several wing-body combinations [R] . Smith, Donald W, Shibata, Harry H, Selan, Ralph 1952

机译：低纵横比机翼在亚音速和超音速下的升力，阻力和俯仰力矩：对大型雷诺数的研究，研究了几种机翼 - 机体组合的低速特性

An engineering method for modeling the interaction of circular bodies and very low aspect ratio cruciform wings at supersonic speeds

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