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Numerical simulations for transonic aerodynamic flows

โœ Scribed by Yau Shu Wong; Hong Jiang


Publisher
Elsevier Science
Year
1991
Tongue
English
Weight
621 KB
Volume
65
Category
Article
ISSN
0010-4655

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โœฆ Synopsis


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 transonic small-disturbance equation, which is a nonlinear and mixed elliptic-hyperbolic partial-differential equation. A Newton-like iterative scheme is developed for solving the transonic equation, and it is used in conjunction with a preconditioned minimal-residual algorithm. The numerical technique is proven to be efficient and reliable. Computational results for transonic flows around the ONERA M6 wing are presented.


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