2016
DOI: 10.1016/j.actaastro.2016.07.029
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The influence of the elastic vibration of the carrier to the aerodynamics of the external store in air-launch-to-orbit process

Abstract: The separation between the carrier and store is one of the most important and difficult phases in Air-launch-to-orbit technology. Based on the previous researches, the interference aerodynamic forces of the store caused by the carrier are obvious in the earlier time during the separation. And the interference aerodynamics will be more complex when considering the elastic deformation of the carrier. Focusing on the conditions that in the earlier time during the separation, the steady and unsteady interference a… Show more

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Cited by 13 publications
(7 citation statements)
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“…22 Therefore, the weighted distance morphing method is used in our code. We have also successfully applied this method in Yang and Ye, 19 Yang et al, 20 and Hua et al 21 The weighted distance method with the establishment of a special weighting function is employed to distribute the displacements of surfaces. The interpolation function is expressed as…”
Section: Mesh Deformation Methodsmentioning
confidence: 99%
See 2 more Smart Citations
“…22 Therefore, the weighted distance morphing method is used in our code. We have also successfully applied this method in Yang and Ye, 19 Yang et al, 20 and Hua et al 21 The weighted distance method with the establishment of a special weighting function is employed to distribute the displacements of surfaces. The interpolation function is expressed as…”
Section: Mesh Deformation Methodsmentioning
confidence: 99%
“…The URANS equations are solved in the CFD simulation, while the modal method has been adopted in the CSD simulation. The in-house code has been successfully applied in Yang and Ye, 19 Yang et al., 20 and Hua et al. 21…”
Section: Methodsmentioning
confidence: 99%
See 1 more Smart Citation
“…8,30 The in-house CFD solver GFSI is used to solve the Euler equations, which has been fully tested for fluid-structure simulations in our previous works. 42,43,46,47 The integral form of the Euler equations can be written as:where W=[ρ,ρu,ρv,ρw,e]T is the vector of conservative variables, p is the density, u, v, and w are the velocity components in x, y, and z directions, and e is the internal energy per unit mass. F(W,Vgrid) is the inviscid flux vector.…”
Section: Methodsmentioning
confidence: 99%
“…In the current research, an in-house code called Generalized Fluid-Structure Interaction, based on the coupled CFD/CSD method, is used to simulate the aeroelastic response of panel flutter induced by oblique shock impingement. The in-house code has been extensively validated and calibrated using real experimental data in previous studies, [41][42][43] and the result of the code has also been compared to other solvers such as Fluent 43 and CFL3D. 44 The aerodynamic loads governed by Euler equations are solved in the CFD simulation, while the nonlinear structure response described by von Kármán's large deflection plate theory is solved based on Galerkin's method in the Computational Structural Dynamics simulation.…”
Section: Methodsmentioning
confidence: 99%