Computational methods of missile aerodynamics

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...

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Bibliographic Details
Main Authors: Atta, E. H., Yeung, Wai Hung.
Other Authors: School of Mechanical and Production Engineering
Format: Research Report
Published: 2008
Subjects:
Online Access:http://hdl.handle.net/10356/6836
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Institution: Nanyang Technological University