한국전산유체공학회:학술대회논문집
- 2006.05a
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- Pages.301-305
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- 2006
Numerical Simulations of the Supersonic Jet Impingement in a Confined Plenum of Vertical Launching System
- Lee Kwang-Seop (Missile Aerodynamics Team Agency for Defence Development(ADD)) ;
- Lee Jin-Gyu (Missile Aerodynamics Team Agency for Defence Development(ADD)) ;
- Hong Seung-Kyu (Missile Aerodynamics Team Agency for Defence Development(ADD)) ;
- Ahan Chang-Soo (Missile Aerodynamics Team Agency for Defence Development(ADD))
- Published : 2006.05.01
Abstract
The Vertical Launching System design is especially complicated by complex flow structure in a plenum with the severe thermal state and high pressure load form the hot exhaust plume. The flow structures are numerically simulated by using the commercial code, CFD-FASTRAN with the axi-symmetrical Navier-Stokes equations. Two different cases are considered; that is, the stationary fire and the moving fire.
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