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Length 11.63 m
Wingspan 18.92 m
Wing Area 88.59 m2
Height 3.1 m
Empty Weight 6350 kg
MTOW 20215 kg
Engine P&W F100-220U
Cruise Speed Mach 0.9 + (subsonic)
Range 3889 + km
Service Ceiling 50,000 t
2 Weap!ns "ays 2000 kg
L#$ 23
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%aria&le %alue 'nits mpty Weight "reakd!(n
We 6350 kg )uselage 0.31
Wp 2000 kg Wings 0.23
W 11865 kg H*tails 0
W+ 20215 kg %*tails 0
'ndercarriage 0.09
Mass )racti!ns Engines 0.13
We#W! 31% Cre( 0
Wp#W! 10% Miscellane!us 0.2
W##W! 59% 1
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)uselage ,Structural- 0.6 .+/.
Empennage 0 +
Engines 0.13 0211
Wings ,Structural- 0.23 3./+1
1 /41+
We/Wo
Wp/Wo
Wf//Wo
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Weight 20215 kg
Wing Area 88.59 m2
Lit C!e Take*!5 0.19019
$ensity 1.225
6ravitait!nal acc 9.81 m/s2
Take O5 $istance 600 ms2
Take O5 Speed 50 m/s
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Landing dist !00
)ricti!n C!e 0.01
6ravitati!nal C!nst 9.81
$ensity 1.225
Landing Speed 55 ms2
Wing SA 88.59
Ma7 Cl in landing c!n8g 0.12315!
MLW 20215
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Thrust Lapse Rate 0.35
Ac -0.05688
9c 9120.16
" 0.06!16
Air density 0.198
Cruise %el!city 306 ms
Aspect Rati! 5.!8
Os(alds E:cieny 0.82
L#$ 23
Cd 0.0106!2
Lit 198309.2 N
Cl 0.256
Wing Area 88.59 m2
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Clim& Angle 0.02618 rad
L#$ 11.5
T#W 0.113136
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F100 PW 220E (Non Afterbuner Variant)
Diameter 0!! m
Engine Weig"t 1#$% kg
&a' "rust $# *N
+F, 0%- .b/.bf"
0000020%-2
00%#$-2 kg/N
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Weights
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40!
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;nputs * Su&s!nic
Airrame
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$istances
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Outputs
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)ueslage $etails Wing 3 ,Elev!ns-
)uselage Length >m? 11.63 R!!t Ch!rd >m? 11.63
)uselage Width >m? 1.2 Tip Ch!rd >m? 3
)uselage Height >m? 3.1 S(eep >deg? 8
C6 ! aircrat >m? .8!2!66 Semi Span >m? .5
AC * 7 ! aircrat >m? 5.65 $ihedral >deg? 2
;ncidence >deg? 0
Output $ata LE * 7 >m? 0
LE * y >m? 0
92.92 LE * @ >m? -0.35
0.00 SMC >m? !.32
%*Tail Area >m2? 0.00 Taper Rati! 0.26
92.92 MAC >m? 8.16
32.92
Aspect Rati! ! Wings 3.8
Aspect Rati! ! H*Tail "#$0' A, #!-2#
C!nstraints T!tal Area >m2?
Wing Area >m2?
H*Tail Area >m2?
Actual Area >m2?
Area >m2?
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Wing Lay!ut
Wing 2 ,Ailer!ns- Wing 4 ,Tip- Wing .
R!!t Ch!rd >m? 3 R!!t Ch!rd >m? 3.01 R!!t Ch!rd >m?
Tip Ch!rd >m? 3.01 Tip Ch!rd >m? 0.2 Tip Ch!rd >m?
S(eep >deg? 25 S(eep >deg? 55 S(eep >deg?
Semi Span >m? Semi Span >m? 0.95 Semi Span >m?
$ihedral >deg? 2 $ihedral >deg? 2 $ihedral >deg?
;ncidence >deg? 0 ;ncidence >deg? 0 ;ncidence >deg?
LE * 7 >m? !.16 LE * 7 >m? 9.02 LE * 7 >m?
LE * y >m? .50 LE * y >m? 8.50 LE * y >m?
LE * @ >m? -0.19 LE * @ >m? -0.05 LE * @ >m?
SMC >m? 3.01 SMC >m? 1.61 SMC >m? """
Taper Rati! 1.00 Taper Rati! 0.0! Taper Rati! """
MAC >m? 3.01 MAC >m? 2.01 MAC >m? """
12.02 1.52 0.00
0$%1$!!-#!#
Area >m2? Area >m2? Area >m2?
)r!nt %ie(
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Wing 1 Wing / Wing
R!!t Ch!rd >m? R!!t Ch!rd >m? R!!t Ch!rd >m?
Tip Ch!rd >m? Tip Ch!rd >m? Tip Ch!rd >m?
S(eep >deg? S(eep >deg? S(eep >deg?
Semi Span >m? Semi Span >m? Semi Span >m?
$ihedral >deg? $ihedral >deg? $ihedral >deg?
;ncidence >deg? ;ncidence >deg? ;ncidence >deg?
LE * 7 >m? LE * 7 >m? 1.5 LE * 7 >m?
LE * y >m? LE * y >m? !.!5 LE * y >m?
LE * @ >m? LE * @ >m? 0 LE * @ >m?
SMC >m? """ SMC >m? """ SMC >m?
Taper Rati! """ Taper Rati! """ Taper Rati!
MAC >m? """ MAC >m? """ MAC >m?
0.00 0.00Area >m2? Area >m2? Area >m2?
Let
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H!ri@!ntal Tail %ertical Tail
R!!t Ch!rd >m? R!!t Ch!rd >m?
Tip Ch!rd >m? Tip Ch!rd >m?
S(eep >deg? S(eep >deg?
Semi Span >m? Semi Span >m?
$ihedral >deg? $ihedral >deg? 0
;ncidence >deg? ;ncidence >deg? 0
LE * 7 >m? LE * 7 >m?
LE * y >m? LE * y >m?
LE * @ >m? LE * @ >m?
"#$0' SMC >m? """ SMC >m? """
"#$0' Taper Rati! """ Taper Rati! """
"#$0' MAC >m? """ MAC >m? """
0.00 0.00 0.00Area >m2? Area >m2?
Hand Side %ie(
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6raph C!!rdinates
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. 0.00 0.00 0.00 """
1 0.00 0.00 0.00 """
AC "#$0' "#$0' "#$0' """
Wing /
3#. Ch!rd Line A 1.50 !.!5 -!.!5 0.00
3#. Ch!rd Line " 1.50 !.!5 -!.!5 0.00
3 1.50 !.!5 -!.!5 """
2 1.50 !.!5 -!.!5 0.004 1.50 !.!5 -!.!5 0.00
. 1.50 !.!5 -!.!5 """
1 1.50 !.!5 -!.!5 """
AC "#$0' "#$0' "#$0' """
Wing
3#. Ch!rd Line A 0.00 0.00 0.00 0.00
3#. Ch!rd Line " 0.00 0.00 0.00 0.00
3 0.00 0.00 0.00 """
2 0.00 0.00 0.00 0.00
4 0.00 0.00 0.00 0.00
. 0.00 0.00 0.00 """1 0.00 0.00 0.00 """
AC "#$0' "#$0' "#$0' """
H*Tail
3#. Ch!rd Line A 0.00 0.00 0.00 0.00
3#. Ch!rd Line " 0.00 0.00 0.00 0.00
3 0.00 0.00 0.00 """
2 0.00 0.00 0.00 0.00
4 0.00 0.00 0.00 0.00
. 0.00 0.00 0.00 """
1 0.00 0.00 0.00 """
AC "#$0' "#$0' "#$0' """
%*Tail
3#. Ch!rd Line A 0.00 0.00 0 0.00
3#. Ch!rd Line " 0.00 0.00 0 0.00
3 0.00 0.00 0.00 0.00
2 0.00 0.00 0.00 0.00
4 0.00 0.00 0 0.00
. 0.00 0.00 0 0.00
1 0.00 0.00 0.00 0.00
AC "#$0' "#$0' "#$0' """
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Parameter +mbo. Va.ue arget Va.ue
:oad distribution # 40$$$$$$$$$% 0%40
+tati de=etion # 0#%%2!% 01
>a.ane * 4002!!%00$ 0%
Damping 8atio # 0-#1$2-1% 0%
Natura. Fre?uen F ###!20-0! - 4 10 rad/s
Damping &ain #$00
Damping Nose n 1000
Nose gear /n -
&ain gear / %
,; Position /c
&ass M 202100
Weig"t M 1!-01
+ti@ness Nose n #$000
+ti@ness &ain -#000
Pre.oad &ain P 4--012
Pre.oad Nose Pn 1$2%$2
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