AIRCRAFT WITH CANARD

• 1. 一种机场用小型飞机乘坐模拟检测系统 [P] . 中国专利： CN110085088B . 2021.01.26
• 2. 基于VR的飞机乘坐体验系统及其使用方法 [P] . 中国专利： CN112613172A . 2021-04-06
• 3. AIRCRAFT OF FEATHERED CANARD ARRANGEMENT (KRASNOV-CANARD) [P] . 俄罗斯专利： RU2609644C1 . 2017-02-02

  机译： 羽绒鸭编的飞机（KRASNOV-CANARD）

• 4. ASSEMBLY AND METHOD FOR OPERATING ROTATABLE MEMBER AROUND ROTARY SHAFT ROTATABLY, AIRCRAFT, ASSEMBLY FOR CONTROLLING AIRCRAFT, AND CANARD ASSEMBLY FOR AIRCRAFT [P] . 日本专利： JP2004323012A . 2004-11-18

  机译： 用于在旋转轴，飞机，控制飞机的组件以及用于飞机的卡纳德组件周围的可旋转构件的组件和方法

• 5. Aircraft systems and canard assemblies for aircraft [P] . 日本专利： JP4319004B2 . 2009-08-26

  机译： 飞机系统和飞机的鸭嘴组件

• 1. THE CANARD-WING INTERFERENCE AND STALL SAFETY OF LIGHT CANARD AIRCRAFT [J] . 中国航空学报：英文版 . 1991,第002期
• 2. China Aircraft Services sets up new aircraft maintenance hangar at HKIA [J] . 无 中国对外贸易：英文版 . 2009,第011期
• 3. A Calculation Method of Rolling Characteristics of Canard Missile with Free-Spinning Tails [J] . Pingan Liu, Mingyuan Liu 哈尔滨工业大学学报（英文版） . 2019,第006期
• 4. Influence of control strategy on stability of dual-spin projectiles with fixed canards [J] . Yu Wang, Xiao-ming Wang, Ji-yan Yu 兵工学报（英文版） . 2018,第006期
• 5. Modeling and Stability Analysis for Dual-Spinning Projectiles with Canards [J] . GUAN Jun, LI Xinhua, YI Wenjun, 东华大学学报（英文版） . 2017,第005期
• 6. Optimal and Robust Solutions for Longitudinal Flight Control of a Canard-Configured High Performance Aircraft [C] . Fatima Shoaib, M. Arsalan Khawaja, Hafiz Zeeshan Iqbal Khan, International Bhurban Conference on Applied Sciences and Technology . 2019
• 7. CFD Investigation of the Drag Effects on an Aircraft by Means of Altering the Wing or Canard Size and Position [D] . Brown, Taylor. 2021
• 8. Lettre à la rédaction: Entérite à virus du canard. Observation au Québec dune condition pathologique ressemblan à la peste du canard [O] . G Bernier, R Filion 1975
• 9. Vortex Dynamics Study and Flow Visualization on Aircraft Model with Different Canard Configurations [O] . Setyawan Bekti Wibowo, Budi Basuki, Tri Agung Rohmat, 2021
• 10. EFFECT OF CANARD LOCATION AND SIZE ON CANARD-WING INTERFERENCE AND AERODYNAMIC-CENTER SHIFT RELATED TO MANEUVERING AIRCRAFT AT TRANSONIC SPEEDS [R] . Blair B. Gloss 1974

• 1. 飞机制造中的IBOM——从干线飞机应用看新支线飞机IBOM的建立 [C] . 杨超凡 . 2002年航空制造技术学术交流会 . 2002
• 2. 主位述位理论在《CVN飞机甲板和机房手册 美国海军航母舰载飞机起飞标准》英汉翻译实践中的应用 [A] . 孙宇翔 . 2018