Device for the indication of the turbulence - vera end, on which the thickening of the boundary layer of a air velocity by means of the supporting surface of an aircraft accompany

• 1. 一种用于湍流边界层流动控制的合成射流装置 [P] . 中国专利： CN113107820A . 2021-07-13
• 2. 一种飞机尾端支撑装置 [P] . 中国专利： CN209939000U . 2020.01.14
• 3. device for the display of the turbulence changes in relation which the thickening of the boundary layer of a luftstroemung on the tragflaeche an aircraft escort [P] . 德国专利： DE000001107975A . 1961-05-31

  机译： 用于显示湍流变化的装置，与护航飞机上的护翼边界层的加厚有关

• 4. Device for repressing of turbulences at the ends of the supporting surfaces of aircraft [P] . 德国专利： DE2434516A1 . 1975-12-04

  机译： 用于抑制飞机支撑面末端的湍流的装置

• 5. Device for the boundary layers influencing to the aircraft supporting force flue [P] . 德国专利： DE729879C . 1943-01-04

  机译： 用于影响飞机支撑力烟道的边界层的装置

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• 6. The Multi-Purpose Airborne Sensor Carrier MASC-3 for Wind and Turbulence Measurements in the Atmospheric Boundary Layer [O] . Alexander Rautenberg, Martin Schön, Kjell zum Berge, 2019
• 7. Experimental review of devices to artificially thicken wind tunnel boundary layers [O] . Sargison JE, Walker GJ, Bond V, 2004
• 8. Investigation of the Feasibility of Active Boundary Layer Thickening for Aircraft Drag Reduction [R] . Ash, R. L., Koodalattupuram, C. 1986

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• 2. Boundary Layer Development on a Concave Surface： Flow Visualization and Hot Wire Velocity Measurements [J] . Farouk Hachem ,Mahmoud Khaled ,Mohamad Ramadan . 能源与动力工程 . 2014,第007期
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• 4. 准周期弹性支撑蒙皮湍流边界层减阻特性研究 [A] . 魏俊东 . 2020