Calculation of Unsteady Transonic Aerodynamics for Oscillating Wings with Thickness
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چکیده
منابع مشابه
Unsteady Transonic Aerodynamic Analysis for Oscillatory Airfoils and Oscillating Flaps Using Dynamic Mesh
This paper presents an algorithm for unsteady transonic aerodynamic analysis by solving the two-dimensional unsteady Euler equations using a dynamic mesh algorithm. The driving algorithm is an upwind biased implicit second order accurate cell-centered finite volume scheme. The spatial discretization technique involves a naturally dissipative flux-split approach that accounts for the local wave ...
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ژورنال
عنوان ژورنال: Journal of Aircraft
سال: 1974
ISSN: 0021-8669,1533-3868
DOI: 10.2514/3.60396