Author(s): T. Anbarasan, Dr. R. Rajasekar
Published in: International Journal of Engineering Research & Technology
License: This work is licensed under a Creative Commons Attribution 4.0 International License.
Volume/Issue: Volume. 6 - Issue. 06 , June - 2017
In this paper presented by predictions of separation moments off the external store weapons carried out on fighter aircraft wing under the Mach number subsonic to supersonic speed. An aerodynamically analysis of static steady condition for Navier-Stoke Equations condition applied on boundary conditions. After that analysis for flow field and shear force acting on stores outer surface area.
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