Computational methods of missile aerodynamics.
Atta, E. H.
Yeung, Wai Hung.
Date of Issue1993
School of Mechanical & Production Engineering
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.
Nanyang Technological University