Development of a New Flap for a Light Utility Transport Aircraft

机译：轻型多用途运输飞机的新型襟翼的开发

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1. Flap failure and aircraft controllability: Developments in asymmetry monitoring techniques [J] . Borello Lorenzo, Villero Giuseppe, Dalla Vedova Matteo D. L. Journal of Mechanical Science and Technology . 2014,第11期

机译：襟翼故障和飞机可控性：不对称监测技术的发展
2. ENFICA-FC: Design of transport aircraft powered by fuel cell & flight test of zero emission 2-seater aircraft powered by fuel cells fueled by hydrogen [J] . G. Romeo, F. Borello, G. Correa, International journal of hydrogen energy . 2013,第1期

机译：ENFICA-FC：由燃料电池驱动的运输机的设计和由氢燃料电池驱动的零排放两人座飞机的飞行测试
3. EXPERIMENTAL INVESTIGATIONS OF EXTERNALLY BLOWN FLAP EFFICIENCY ON THE MODEL OF SHORT TAKEOFF AND LANDING TWIN-ENGINE TRANSPORT AIRCRAFT [J] . Albert Vasilievich Petrov, Evgeny Alexandrovich Pigusov TsAGI science journal . 2019,第2期

机译：短程起降双引擎运输飞机模型外部吹气襟翼效率的实验研究
4. DEVELOPING A NEW FLAP FOR A LIGHT UTILITY TRANSPORT AIRCRAFT [C] . B. Eggleston, W.D. McKinney, J. Banaszek, 23rd international congress of aeronautical sciences (ICAS 2002) . 2002

机译：为轻型运输飞机开发新的襟翼
5. Development and flight test of a multi-function controller for automated cruise flaps on an aircraft wing [D] . Cox, Craig Allen 2008

机译：飞机机翼自动巡航襟翼多功能控制器的开发和飞行测试
6. Special forms of flight. III: Supersonic transport aircraft. [O] . F J Mills, R M Harding 1983

机译：特殊的飞行形式。三：超音速运输机。
7. DESIGN, DEVELOPMENT AND VALIDATION OF FIRE PROTECTIONudSCHEME FOR THE ENGINE FIREWALLS AND COWLING OFudA TYPICAL LIGHT TRANSPORT AIRCRAFT [O] . Akshatha HT, Rinku A, Gopalakrishnan R 2014

机译：防火设计，开发和验证 ud引擎防火墙和 ud的耦合方案典型的轻型运输飞机
8. Coupled Vortex-Lattice Flight Dynamic Model with Aeroelastic Finite-Element Model of Flexible Wing Transport Aircraft with Variable Camber Continuous Trailing Edge Flap for Drag Reduction [R] . Nguyen, N, Ting, E, Nguyen, D, 2013

机译：具有可变弯曲连续后缘襟翼的柔性翼运输飞机气动弹性有限元模型耦合涡旋 - 格子飞行动力学模型

Development of a New Flap for a Light Utility Transport Aircraft

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