Outlet nozzles device for aircraft with jet propulsion engine

• 1. 由带有反转的风扇的涡轮喷气发动机推进的飞机 [P] . 中国专利： CN104781143B . 2017.09.01
• 2. 由带有反转的风扇的涡轮喷气发动机推进的飞机 [P] . 中国专利： CN104781143A . 2015-07-15
• 3. AN OUTLET NOZZLE FOR A JET ENGINE, AN AIRCRAFT COMPRISING THE OUTLET NOZZLE AND A METHOD FOR CONTROLLING A GAS FLOW FROM THE JET ENGINE [P] . 欧洲知识产权局专利： EP1809888A4 . 2013-05-15

  机译： 喷气发动机的出口喷嘴，包括出口喷嘴的飞机和控制喷气发动机气流的方法

• 4. Outlet nozzle for a jet engine, an aircraft comprising the outlet nozzle and a method for controlling a gas flow from the jet engine [P] . 美国专利： US8327617B2 . 2012-12-11

  机译： 用于喷气发动机的出口喷嘴，包括该出口喷嘴的飞机以及用于控制来自喷气发动机的气流的方法

• 5. AN OUTLET NOZZLE FOR A JET ENGINE, AN AIRCRAFT COMPRISING THE OUTLET NOZZLE AND A METHOD FOR CONTROLLING A GAS FLOW FROM THE JET ENGINE [P] . 美国专利： US2007271901A1 . 2007-11-29

  机译： 喷气发动机的出口喷嘴，包括出口喷嘴的飞机和控制喷气发动机气流的方法

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• 6. EFFECT OF COMPRESSOR-OUTLET AIR BLEED ON PERFORMANCE OF A CENTRIFUGAL-FLOW TURBOJET ENGINE WITH AnCONSTANT-AREA JET NOZZLE [R] . Sidney C. Huntley 1952

• 1. Numerical Analysis and Verification of the Gas Jet from Aircraft Engines Impacting a Jet Blast Deflector [J] . Fu-Dong Gao ,De-Xin Wang ,Hai-Dong Wang . 中国机械工程学报 . 2018,第005期
• 2. Computational Analysis of Flow Field on the Propulsion Nozzle of a Micro-Turbojet Engine [J] . Jorge Luis Garrido-Téllez ,Miguel Toledo-Velázquez ,Samuel Alcántara-Montes . 工程（英文）（1947-3931） . 2012,第1期
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