Separation simulation studies of large disturbance and high speed at low altitude

Based on the secondary development function of ADAMS/VIEW, a parameterized simulation model of aircraft separation simulation is established by the external Fortran subroutine. A five-dimensional aerodynamic matrix is established in the program. The fourdimensional interpolation algorithm is used to...

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Veröffentlicht in:	Journal of physics. Conference series 2019-10, Vol.1324 (1), p.12066
Hauptverfasser:	Fan, Siyi, Fei, Wanghua, Guo, Pengfei, Zhang, Xuan, Yin, Geling, Zhang, Weiqiang, Shi, Rui, Ma, Ye
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerodynamic forces Aerodynamics Aircraft Algorithms Angle of attack Angular velocity Dynamic models Interpolation Low altitude Moments of inertia Parameterization Physics Pitch (inclination) Rolling motion Separation Sideslip Simulation Yaw
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