Computational methods of missile aerodynamics

• المؤلفون الرئيسيون: Atta, E. H., Yeung, Wai Hung.
• مؤلفون آخرون: School of Mechanical and Production Engineering
• التنسيق: Research Report
• منشور في: 2008
• الموضوعات: DRNTU::Engineering::Aeronautical engineering::Aerodynamics
• الوصول للمادة أونلاين: http://hdl.handle.net/10356/6836
• المؤسسة: Nanyang Technological University

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...