Special Publication of National Aerospace Laboratory SP-16
巻
16
ページ
283 - 288
発行年
1991-12
抄録（英）
The flow fields over interior and exterior of simplified SCRAM jet model are simulated numerically by 2-Dimensional Navier-Stokes equations using an implicit finite difference scheme. For these simulations, the numerical scheme based on Chakravarthy-Osher's TVD formulation is improved for multi grid application and Simple & Robust wall boundary conditions are applied. In this paper, the computed results are compared with two kinds of experiments, one is conducted by high speed wind tunnel and the other is conducted by hydraulic tank.
スクラムジェット内流の数値シミュレーション
nalsp0016045.pdf
(605.89KB)
