Skip to content

Commit 9c9bf17

Browse files
planesplanes
committed
faster regional jet
1 parent cf8d501 commit 9c9bf17

File tree

9 files changed

+788
-14
lines changed

9 files changed

+788
-14
lines changed

‎B737_AVL_Tutorial/avl_files/Boeing_737-800.avl‎

Lines changed: 169 additions & 0 deletions
Original file line numberDiff line numberDiff line change
@@ -0,0 +1,169 @@
1+
base
2+
3+
#Mach
4+
0.0
5+
6+
#Iysym IZsym Zsym
7+
0 0 0.0
8+
9+
#Sref Cref Bref <meters>
10+
124.862 4.235 34.32
11+
12+
#Xref Yref Zref <meters>
13+
0.0 0.0 0.0
14+
15+
16+
17+
#---------------------------------------------------------
18+
SURFACE
19+
main_wing
20+
#Nchordwise Cspace Nspanwise Sspace
21+
10 1.0 20 1.0
22+
23+
YDUPLICATE
24+
0.0
25+
26+
27+
SECTION
28+
#Xle Yle Zle Chord Ainc Nspanwise Sspace
29+
13.61 0 -1.27 7.76 0.0698
30+
31+
SECTION
32+
#Xle Yle Zle Chord Ainc Nspanwise Sspace
33+
21.6118 17.16 -1.27 0.782 0.0
34+
35+
36+
#---------------------------------------------------------
37+
SURFACE
38+
horizontal_stabilizer
39+
#Nchordwise Cspace Nspanwise Sspace
40+
10 1.0 20 1.0
41+
42+
YDUPLICATE
43+
0.0
44+
45+
46+
SECTION
47+
#Xle Yle Zle Chord Ainc Nspanwise Sspace
48+
32.83 0 1.14 4.7 0.0524
49+
50+
SECTION
51+
#Xle Yle Zle Chord Ainc Nspanwise Sspace
52+
38.7876 7.1 1.14 0.955 0.0524
53+
54+
55+
#---------------------------------------------------------
56+
SURFACE
57+
vertical_stabilizer
58+
#Nchordwise Cspace Nspanwise Sspace
59+
10 1.0 20 -1.1
60+
61+
SECTION
62+
#Xle Yle Zle Chord Ainc Nspanwise Sspace
63+
28.79 0 1.54 8.19 0.0
64+
65+
SECTION
66+
#Xle Yle Zle Chord Ainc Nspanwise Sspace
67+
32.4165 0.0 9.317 0.95 0.0
68+
69+
70+
#---------------------------------------------------------
71+
SURFACE
72+
fuselage_horizontal
73+
#Nchordwise Cspace Nspanwise Sspace
74+
10 1.0
75+
76+
SECTION
77+
#Xle Yle Zle Chord Ainc Nspanwise Sspace
78+
6.4 -1.87 0.0 23.62 0.0 1 0
79+
80+
SECTION
81+
#Xle Yle Zle Chord Ainc Nspanwise Sspace
82+
3.6461 -1.496 0.0 29.5714 0.0 1 0
83+
84+
SECTION
85+
#Xle Yle Zle Chord Ainc Nspanwise Sspace
86+
2.1944 -1.122 0.0 32.8478 0.0 1 0
87+
88+
SECTION
89+
#Xle Yle Zle Chord Ainc Nspanwise Sspace
90+
1.1408 -0.748 0.0 35.2774 0.0 1 0
91+
92+
SECTION
93+
#Xle Yle Zle Chord Ainc Nspanwise Sspace
94+
0.3925 -0.374 0.0 37.0465 0.0 1 0
95+
96+
SECTION
97+
#Xle Yle Zle Chord Ainc Nspanwise Sspace
98+
0.0 0.0 0.0 38.02 0.0 1 0
99+
100+
SECTION
101+
#Xle Yle Zle Chord Ainc Nspanwise Sspace
102+
0.3925 0.374 0.0 37.0465 0.0 1 0
103+
104+
SECTION
105+
#Xle Yle Zle Chord Ainc Nspanwise Sspace
106+
1.1408 0.748 0.0 35.2774 0.0 1 0
107+
108+
SECTION
109+
#Xle Yle Zle Chord Ainc Nspanwise Sspace
110+
2.1944 1.122 0.0 32.8478 0.0 1 0
111+
112+
SECTION
113+
#Xle Yle Zle Chord Ainc Nspanwise Sspace
114+
3.6461 1.496 0.0 29.5714 0.0 1 0
115+
116+
SECTION
117+
#Xle Yle Zle Chord Ainc Nspanwise Sspace
118+
6.4 1.87 0.0 23.62 0.0 1 0
119+
120+
121+
#---------------------------------------------------------
122+
SURFACE
123+
fuselage_vertical
124+
#Nchordwise Cspace Nspanwise Sspace
125+
10 1.0
126+
127+
SECTION
128+
#Xle Yle Zle Chord Ainc Nspanwise Sspace
129+
6.4 0.0 -1.87 23.62 0.0 1 0
130+
131+
SECTION
132+
#Xle Yle Zle Chord Ainc Nspanwise Sspace
133+
3.6461 0.0 -1.496 29.5714 0.0 1 0
134+
135+
SECTION
136+
#Xle Yle Zle Chord Ainc Nspanwise Sspace
137+
2.1944 0.0 -1.122 32.8478 0.0 1 0
138+
139+
SECTION
140+
#Xle Yle Zle Chord Ainc Nspanwise Sspace
141+
1.1408 0.0 -0.748 35.2774 0.0 1 0
142+
143+
SECTION
144+
#Xle Yle Zle Chord Ainc Nspanwise Sspace
145+
0.3925 0.0 -0.374 37.0465 0.0 1 0
146+
147+
SECTION
148+
#Xle Yle Zle Chord Ainc Nspanwise Sspace
149+
0.0 0.0 0.0 38.02 0.0 1 0
150+
151+
SECTION
152+
#Xle Yle Zle Chord Ainc Nspanwise Sspace
153+
0.3925 0.0 0.374 37.0465 0.0 1 0
154+
155+
SECTION
156+
#Xle Yle Zle Chord Ainc Nspanwise Sspace
157+
1.1408 0.0 0.748 35.2774 0.0 1 0
158+
159+
SECTION
160+
#Xle Yle Zle Chord Ainc Nspanwise Sspace
161+
2.1944 0.0 1.122 32.8478 0.0 1 0
162+
163+
SECTION
164+
#Xle Yle Zle Chord Ainc Nspanwise Sspace
165+
3.6461 0.0 1.496 29.5714 0.0 1 0
166+
167+
SECTION
168+
#Xle Yle Zle Chord Ainc Nspanwise Sspace
169+
6.4 0.0 1.87 23.62 0.0 1 0

‎B737_AVL_Tutorial/avl_files/Boeing_737-800.mass‎

Lines changed: 32 additions & 0 deletions
Original file line numberDiff line numberDiff line change
@@ -0,0 +1,32 @@
1+
2+
#-------------------------------------------------
3+
# Boeing_737-800
4+
#
5+
# Dimensional unit and parameter data.
6+
# Mass & Inertia breakdown.
7+
#-------------------------------------------------
8+
9+
# Names and scalings for units to be used for trim and eigenmode calculations.
10+
# The Lunit and Munit values scale the mass, xyz, and inertia table data below.
11+
# Lunit value will also scale all lengths and areas in the AVL input file.
12+
Lunit = 1.0 m
13+
Munit = 1.0 kg
14+
Tunit = 1.0 s
15+
16+
#-------------------------
17+
# Gravity and density to be used as default values in trim setup.
18+
# Must be in the units given above.
19+
g = 9.81
20+
rho = 1.2250000002007604
21+
22+
#-------------------------
23+
# Mass & Inertia breakdown.
24+
# x y z is location of item's own CG.
25+
# Ixx... are item's inertias about item's own CG.
26+
#
27+
# x,y,z system here must be exactly the same one used in the AVL input file
28+
# (same orientation, same origin location, same length units)
29+
#
30+
# mass x y z Ixx Iyy Izz Component Name
31+
#
32+
79015.8 0.0 0.0 0.0 0.0 0.0 0.0 ! Boeing_737-800

0 commit comments

Comments
 (0)