Simulation of Store Separation using Low-cost CFD with Dynamic Meshing

Publish Year: 1393
نوع سند: مقاله ژورنالی
زبان: English
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شناسه ملی سند علمی:

JR_IJE-27-5_006

تاریخ نمایه سازی: 17 خرداد 1393

Abstract:

The simulation of the store separation using the automatic coupling of dynamic equations with flow aerodynamics is addressed. The precision and cost (calculation time) were considered as comparators.The method used in the present research decreased the calculation cost while limiting the solution errorwithin a specific and tolerable interval. The methods applied to model the aerodynamic forces are timedependent dynamic meshes and quasi-static methods. In the time-dependent method, a dynamic unstructured tetrahedral mesh approach using combination of spring-based smoothing and localremeshing is employed in respect of bodies motion with an implicit, second-order upwind accurate 3-D Euler solver. In this method, a 6dof dynamic code is coupled with the flow solver to update the store trajectory information. In the quasi-static method, a 3-D implicit, steady state Euler solver isautomatically integrated with a grid generation software and a 6dof dynamic code. Although the timedependentmethod is more precise and reliable, it is not proper and appropriate for the initial design of the separation system due to its high cost. The quasi-static solution is very fast, but unable to simulate realistically because of not satisfying the problem conditions due to solution divergence as the storespeed increases. The method used in the present research decreased the calculation cost while limiting the solution error within a specific and tolerable interval. In this way, the time step can be enlarged, the solution can be carried out with a few calculation points, and the solution can have considerably morespeed with a limited error magnitude. Simulation of the store separation using the automatic coupling of dynamic equations with flow aerodynamics with the new Low-Cost method is the innovative aspect of this paper. To validate the solution method, the transonic store separation was simulated that agreed well with the wind tunnel test outcomes.

Authors

m jafari

Department of New Technologies Engineering, Shahid Beheshti University, Tehran, Iran

a toloei

Department of New Technologies Engineering, Shahid Beheshti University, Tehran, Iran

s ghasemlu

Department of Aerospace Engineering, Amirkabir University, Tehran, Iran

h Parhizkar

Department of Aerospace Engineering, Amirkabir University, Tehran, Iran