期刊论文详细信息
Aviation
Numerical analysis of the impact of sideslip angle on load of the gyrocopter stabilizers
Zbigniew Czyż1  Paweł Karpiński2 
[1] Aeronautics Faculty, Polish Air Force University, 35 Dywizjonu 303 St., 08-521 Dęblin, Poland;Department of Thermodynamics, Fluid Mechanics and Aviation Propulsion Systems, Faculty of MechanicalEngineering, Lublin University of Technology, 36 Nadbystrzycka St., 20-618 Lublin, Poland;
关键词: aerodynamic force;    autogyro;    gyrocopter;    gyroplane;    sideslip angle;    stabilizer;   
DOI  :  10.3846/aviation.2019.11924
来源: DOAJ
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