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Title: Computational methods of missile aerodynamics
Authors: Atta, E. H.
Yeung, Wai Hung.
Keywords: DRNTU::Engineering::Aeronautical engineering::Aerodynamics
Issue Date: 1993
Abstract: A computational method has been developed for the prediction of missile flow fields with emphasis on subsonic and transonic flight-conditions. The computational method is based on the thin shear layer formulation of the Navier-Stokes equations and a finite volume Runge-Kutta time marching algorithm.
Rights: Nanyang Technological University
Fulltext Permission: restricted
Fulltext Availability: With Fulltext
Appears in Collections:MAE Research Reports (Staff & Graduate Students)

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