Computational Fluid Dynamics Modelling of Store Separation for Transonic Generic Store

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2018

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American Institute of Aeronautics and Astronautics Inc, AIAA

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In this study, two different well-known wind tunnel techniques; “Captive Trajectory Method “and “Grid Surveying Method “are simulated using Computational Fluid Dynamics (CFD) method. Time dependent behavior of a generic store during the release process from a delta wing under high transonic flow regime is determined. First of all, in captive trajectory simulation, simultaneous trajectory and attitude computations are accomplished by utilizing a reliable commercial flow solver called ANSYS Fluent. Secondly, aerodynamic grid database generation required for grid surveying approach is performed and the trajectory of the store is determined by using a standalone store separation module built in MATLAB Simulink. The numerical outputs are compared with available wind tunnel results conducted in Arnold Engineering Development Center. © 2018, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.

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0203 mechanical engineering, 0103 physical sciences, 02 engineering and technology, 01 natural sciences

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2018 Fluid Dynamics Conference -- 48th AIAA Fluid Dynamics Conference, 2018 -- 25 June 2018 through 29 June 2018 -- Atlanta -- 215139

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