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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