โ Scribed by Cherry, T. M.
No coin nor oath required. For personal study only.
๐ SIMILAR VOLUMES
In this paper, the conformal mapping technique combined with the algebraic method is used to generate the unified body fitted orthonormal O-H mesh for fighter-type aircraft. The flow field and aerodynamic characteristics of complete aircraft's subsonictransonic-supersonic flow at angles of attack up
Transonic flow is an important aerodynamic phenomenon that occurs in the high subsonic Mach number flight regime. This paper presents the development of a numerical simulation for three-dimensional transonic aerodynamic flows around an isolated wing. The mathematical formulation is based on a transo
In this paper, numerical methods for solving the transonic full potential equation are developed. The governing equation is discretized by a flux-biasing finite volume method. The resulting non-linear algebraic system is solved by using a continuation method with full Newton iteration. The continuat