FLOW-3D_Aerospace_App.pdf

节选段落一：
11 Case 12
Case 7
Case 8
Case 2
Case 9
Case 1
Case 3
Case 10
Case 4
Case 5
Case 11
Case 12
Case 6
0.00
1.00
2.00
3.00
4.00
5.00
6.00
0 10 20 30 40 50 60 70 80
time (s)
t
f
(ft
)
Case 1 Case 2
Case 3 Case 4
Case 5 Case 6
Case 7 Case 8
Case 9 Case 10
Case 11 Case 12
Case 1
Case 2
Case 3
Case 4
Case 5


节选段落二：
Conference, Paper 2007-5524, Cincinnati, Ohio, July 2007.
1.初始条件: 粗略的增压阶段,依据量测数据,找出精准的模拟所需的初始条件
2.增压: 在喷雾前,燃料舱因为外部受热而产生的自我增压
3.


节选段落三：
We greatly thank Flow Science for the dedicated support to
make a CFD-based design process possible for cryogenic
fluid systems in aerospace.