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NTIS 바로가기韓國軍事科學技術學會誌 = Journal of the KIMST, v.26 no.2, 2023년, pp.149 - 158
허기훈 (국방과학연구소 미사일연구원) , 남현재 (국방과학연구소 미사일연구원) , 임경진 (국방과학연구소 미사일연구원) , 이영빈 (국방과학연구소 미사일연구원)
To predict the aerodynamic characteristics of the grid fins from subsonic to supersonic speeds, low fidelity SW as well as CFD SW were applied. VLM(Vortex Lattice Method) and SE(Shock-Expansion) method were used at subsonic and supersonic speed domain respectively for the rapid prediction of low fid...
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