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Effects of varying the size and location of trailing-edge flap-type controls on the aerodynamic characteristics of a unswept wing at a Mach number of 1.9

机译：改变后缘襟翼式控制器的尺寸和位置对马赫数为1.9的未扫掠翼的气动特性的影响

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Mitchell, Meade H , Jr;
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年度 1950
页码 1-35
总页数 35
原文格式 PDF
正文语种 eng
中图分类工业技术;
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2. Effects of Unsteady Trailing-Edge Blowing on Delta Wing Aerodynamics [J] . Ping Jiang, Zhijin Wang, Ismet Gursul Journal of Aircraft . 2010,第2期

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3. Flow Patterns and Aerodynamic Performance of Unswept and Swept-Back Wings [J] . Shun C. Yen, Lung C. Huang Journal of Fluids Engineering: Transactions of the ASME . 2009,第11期

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4. Aerodynamic Optimization of Mach 0.745 Transonic Truss-Braced Wing Aircraft with Variable-Camber Continuous Trailing-Edge Flap [C] . Juntao Xiong, Robert E. Bartels, Nhan Nguyen AIAA SciTech Forum and Exposition . 2021

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5. Unsteady aerodynamic modeling with time-varying free-stream Mach numbers. [D] . Jose, Arun Isaac. 2005

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Effects of varying the size and location of trailing-edge flap-type controls on the aerodynamic characteristics of a unswept wing at a Mach number of 1.9

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