A high efficient method for computing dynamic derivatives of aircraft based on quasi-steady CFD method
This article considers the experiences of engineering design and engineering calculation method, based on the quasi-steady Euler equations to solve arbitrary aerodynamic shape which can be fit for subsonic flow, transonic flow and supersonic flow with high efficient. Compared to the calculation results of the general method with unsteady solution and experimental data, the results show that the method is reliable and efficient.
NETL
NSTL
万方数据
维普
