TABLE' 1.- DIMEaS!Oi'~S OF WIli}S

___ ,'__ _________________________ (li1 __ DE!1~!i~e;s - Dou~le~V{edge Section

ty:-f E;,

-, ~ ~ -,'

:~ 1 L-tl.' T "

~ k-t • - --- t/cmax

-

\'ling E; ). A$pect' t/Cmax, hit, (:r b

(deg) (deg) ratio location (in.) (in. ) -_._", -_ ..

-- -1 9.9 90 0.70 0.08 0.18c 0 4.85 1.70 --2 17.4 90 1.25 .08 .18c 0 5.42 3.39

3 18.1 90 1.31 .08 .5Oc 0 5.98 3.91' 4 29.8 90 2.29 .05 .sOc 0 . 4.98 S.71 -

-5 3h.7 90 2.77 .0S • SOc 0 4.99 6.91 6 39.8 90 ,3.33 .05 . SOc 0 5.00 8.32 7 4S.0 90 4.00 .05 .sOc 0 4.99 9.96

-

(b) De1ta Wings - Variable-Thickn~ss-Ratio ~exagonal Section

1rtT . A-A

•

q~ Jkh (tic) (t/c)tmax . hit

location location e "- Aspect

Wing. (deg) (deg) rat5,o

0.31-. 36Cr 0.Q692 o.692Ct 0.5 .31-.86<;- .0461 O.692ct 0 .30-.87cr .0922 0.692Ct 0 .30-.87 ' .0922 0.692cf 0.5 .30-.8 .0922 O.692ct 1.0

8 10.0 90 0.70 0.03 9 30.0 90 2.31 .C2

10 29.8 ,90 2.29 .04 11 29.8 90 2.29 • ott 12 29.8 90 2.29 .04

i'i

(r ~ / -

/' • I

.. J {

cr (; n \

.......... 1. I

5.80 5.90 5.93 5.93 5.93

/

b (in. )

2.03 6.81 6.78 6.78 6.78

-$

- J'

-6

- I

- /:

if-

f)

b

7

I - I

.' .1 t

I i

.I1'~ pL -

_I J Y1

TABLE 1.- CONCLUDED.

_ (c) D~lta Wings - Constant.-Thiclmess-Ratio ~exC'.gonaJ sp'~tion

t

& ~ Aspect t/cmax

t/cmax cr b Wing (deg) (deg) ratio location hit (. ) (" ) ,In. 1.n. /

'-_ ..

13 29.6 90 2.27 0.0395 0.40-.6.')C 0 5.00 5.68 14 39.9 90 3.35 .0395 .40-.60c 0 4.99 8.31) 15 .44,·7 9Q- 3.96 .0395 -.ho-.&)c 0 4.99 9.89.

...

(d) Diamond \Ving - Variable-'I'hiclmes~-Ra+,i(' Hexaf'r.naJ. Sec-t,i 0n

/ -

& ). Aspect (t/c)r (t/c)r (t/c)t (t/c)~ 0r b Wing (deg) (deg) ratio max hit (j n. ) (in. ) max location max location

. - • 16 29~8 150.2 1.15 0.03 O.30-.87c . r 0.0692 0.692 Ct 0 r:;' ~~ .... /-- 3. J~l_

(e) Arrow Wings - Sin~le-Wedge Secti.-,n

;~I t h

~ • _~ ...... J

Wing & ~ -Aspect

t/c-1MX t/cmax hit

Cr b (deg) (deg) ratio location (in. ) (ir. )

17 25.6 39.6 4.55 o.c6 I.OOc 1.0 2.68 6.10 , 18 30.5 56.4 3.87 .13 l.OOc 1 .~

01./ "l c'? _' • .,J- 6.eO

':1';;.-.£, :it'.

K,

1i TABLE 2.- AERODD-IAMIC CHARACTERISTICS OF WING 1

Aspect Ratio ~ 0.70 tan &, = 0.68 :.\ .... ;:.'11- tan m' '-, ~~ a. CL ,On .Cm ~ C.P. C.P. :t"!..""ri- (deg) (% Or) (% b/2)

- '~ 13.92 0~151 0.041 - -0.0092 0.019 73 13 <' ,

. ' :- .-~~

11.94 .121 .03) . -.0081 .019 73 16

9.95 - .llO • 024 "';'.0051 .039 72 35 l

7.96 .085 .018 -.0045 '72 16 I .0.39 ..

5.97 .068 .016 -.0024 ' .059 70 86

4.97 .055 ' .014 -;.0020 .059 70 " 106

3.98 .043 .013 -.0015 .059 70 135

2.99 ' ' .031 .013 -.COll .040 70 127

1.99 .025 .012 -.0009 .020 70 79 . \0.99 .012 .011 -.0005 .020 71 158

0 .006 .011 .0013 .020

" 0 .006 .Oll .0013 .020 (I:

0 .006 .Oll ' .0025 .020

-.99 -.006 .013 ' .0017 .020 93 319

-1.99 -~012 .013 .0034 .020 94 158

, :-2.98 -.024 .014 .0031 .020 79 79

-3 .. 98 -.037 .014 .0020 .040 72 106

-4.98 -.043 .015 .0038 0 75 0

--5.97 -.049 .017 .0047 0 76 0

-7.96 -.072 " .021 .0063 -.039 75 5.3

-9.95 -.090 .027 .0077 -.039 75 42 ,

!

-11.94 -.108 .033 ' .0091: -.077 75 70

-1.3.93 -.125 .042 .0112 -.116 75 90

L-36P06i

TABLE 3.- AERODYNAMIC CHARACTERISTICS OF WING 2

Aspect Ratio = 1.25 :: : = 1.22 a- CL On Cm 'i> C.P. C.P. (deg) (% Or) (% b/2)

13.84 0.185 0.054 -0.0014 0.056 67 30

11.87 .156 .041 -.0006 .052 67 33

9.90 .133 .033 .0012 .044 66 32

·7.92 .104 .025 • roll .039 .. 66 38

5.95 .074 .019 .. 0010 .035 65 47 -

.4.96 .060 .018 .0008 .027 65 43

3.96 .047 .• 017- .0005 .022 66 47

2.97 .036 .017 .0007 .018 65 36

2 .. 97 .036 .016 .0007 .013 65 49

1.98 .022 .013 .. 0002 .013 66 59

_ '0.99 .on· .013 .000l .009 66 79

0 0 .015- .0003 .004 . -0 0 .016 .0003 .004

-.99 -.on .015 -.0001 0 66

-1.98 -.019 .015 .0003 -.004 68 23

-2.97 -.033 .016 .0001 -.009 68 26

-3.96 -.049 .018. -.0003 -.018 67 35

-4.95 -.060 .020 .0001 -.022 67 36

-5.94 -.073 .. 022 .0002 - -.031 67 4l. -7.92 -.097 .026 .0007 -.039 67 40 -9.89 -.124 .035 .0015 -.056 68 45

-n.87 -.150 .043 .0021 -. 065 68 43

-13.84 -.173 .054 .0030 -.082 68 46

-L-36P067

......

,

f" ;_.,

,........-,.

TABLE t!!:.- }..ERODYNAMIC· CHARACTERISTICS OF ViING 13. L .... '

c

Aspect Ratio = 1.33 tan & = 1.28. ~ ~~

tanm ..

Ct CL CD em Pb . C.P. C.P. (deg)

f~'SlI..--l-,-,-, (0/0 Cr) (0/0 b!2)

'13.86 0.203 0.060 0.0039 -OJ I 0.062' 65 30" .. - 11.88 .047 .0042

i i . .179 i .059 . 65 33 .' I 1

9:90 I

.156 .038 .0050 ,

.OSh: 64 34 I

I

, 7.93 • 125j' .027 • 0045 .045 . 63 36

~ 5.95

, .093 .019 .0033 I .036 • 64 38 .,

i

4.96 .078 .016 ·9029 I .033 63 42 I

I 3.96 .061 .014 .0022

I .027 63 44 ,

'. ;> 2.97 • 046 •. 012 .0018 .02]. ~ . 63 46 [

. " f ,

1.98 .031 .011 .0014 .012 62 39 ~ . ,

.99 .013 .• 011 ' .0008 .005' ':1 0_ 34 ~

\ I: i 0 -.002 .010 .003

;

.0001

.01 -.007 .010 0 .003 ' f

-.98 -.024 .010 -.0006 -.006 1 64 .25

-1.97 -.037 .011 -.0005 -.009 .' 65 24 1'," .. t .

.,...2.96 -.057 .013 -.0014 -.018 64 32

-3.95 -.078 .016 -.0022 -.030 . 64 38 'fA".""

-4.95 -.093 .018 -.0029 -.036 64 38

-.042 r •

-5.93 -.109 .021 -.0030 64 38

-7.92 -.135 .029 -.0041 -.05~ 64 37

-9.89 -.164 .039 -.0047 -.065 64- 39

~1l.87 -~186 .050 -.0044 . -.068 65 36

"':13~84 ·-.208 .062 -.0025 -.082 66 39

L-36P067

L-36P061

. 4 . (deg)"

13.80

1l~83

11.83

.' ~:'86 .7.S9

5.92

4.94

3.95

.2.96

1 .. 98-

.99

o

o

-.99

~1.98

...,2~96

-.3.95

~4.94

-5.92

-7.89

-9.87

-ll.Sh "

-lLSh

-13.81

__ •• ~ _____ ."'_-:_ • -' __ ~" __ -'-_ '_0 __ , ___ ._

Aspect Ratio = 2.31 , tan £

.. :tiin m = 2.26 C.P. ·c.P •

(°/0 crJ (°/0 b/2) CL

0.254

Cn

0.070

.054.

.055

0.0010 67 35'

.221

.223

.188

• 152.

.107

.OS9

.072

.054

.036

.. 020

~OO2

.004

-.016

-.032

-.052

-.074

-.091

-.10S

-.149

~.lS5

-.217

-.215 --.249

.• 040

.02S

.01S

.oi5

.012

.010

.008

.00S·

.007

.007

.007

.008

.010

.013

.015

.019

.029

.042

.055

.055

>'

.0012

.0012

.0018

-.0020

".0012

.0009

.. 0008

.0010

.0007

.,oooS

.0004

.0002

-.0004

-.0004 . -.0004

-.:ooos .'

-.CrOl0

-~OO10

-.OOlS

-.ooiS

-.0012

.015

;.C08

i 0 ' '-

i·":";·~OO2 i'- ,

!-.oo5 t

f_.014 1,·,: . ~ -".'

;-.020 ~ :-.026 t­t-.032 ~: ".

I

67 36 "

67 37

66 38 .

66 38

66 37

66 3S

66 40

65 h4

65 43

63 43

65

66

66

66

66

t-.o41· 66

32

42

39

35

35

38

39

38

39

f" I • ,

t~.059 . ~. 66 j' :-.072 66 t ;-.085 66 t: ~-.087 67 - 40 ,.

" -.0011 - 1-.101 67 40

9.· ..

, ~ --~~~~K~~~~~' i

; ,

"

'TABLE {;1-, AERODYN).}HC ClUL.'tACTERISTICS OF WING \~:; L' .

Aspect Ratio = 2.76 tan & = 2.71 , c tan III

a; CL CD Om Cb C.P. C.P. (deg)

~~-----

(0/0 cr) (0/0 b/2) i [--\~

,13.75 I 0.075 '66 3~ 0.273 ! 0.0009 lO.096

1"-t ~

~084, 1l.79 .231 .056 .0009 t~ .:~j 66 36 ...... 1 ! t

':9.83 .192 .041 .0014 \

.068 66 35

9.83 .191 .040 .0013 \ .070 66 36 ! 1 , I

7.87 .151 .028 .0012 I .055, 66 36 " 1

5.90 .lll .017 '-O~10 .043' 66 I 39 l

4.92 .092 .01.4 .0009 \ .035 66 38

3.94 .074 .012 .0010 .028 65 37

2.96 .055 .010 .0009 .022 65 40

1.97 .037 .009 .0006 ~()14' 65 38

, .99 .019 .008 .co05 .co8, 64 42

0 -.002 .006 .0000 \ .002 - I I

I r - :

-.98 -.018 .007 .0001 i -.005 67 26 , '

-1.97 -.036 .008 -.0002 i" i ';.012 66 32

-2.95 .,...055 .009 ' -.0004 ';:018 66 32 .tj

~3~94 -.071, .012 -.oob2 -~026 66 36

-4.92 -.092 .015 -.0007 .-.033 66 36 I . i, " ,.;0,""

-5.90 -.109 .019 -.0006 r-~039 • 66 36 ;

-7.87 -.150 .028 -.0017 1:-~055 : 65 36

-9.83 -.189 .041 -.0015. 66 37

-9.84 -.191 .041 -.0019 66 36

-1l.79 -.227, .056 -.0011 i-.087 . 66 38 t

-13.75 -.265 4 .074 -.0006 :-.104' 66 - 39 -"-- .- .. -..

.. L-36Pp67 -.--- .. '

.~, .

. -.' -..

c

,.:

'.

0

ct (deg)

13~70

>.11.75

9.80 .'

7.84

.; 5.88

4.90

3 .. 92

2.94 '

1.,98

.98

-.01

0

-.98

-1.96

.;.2.95 ..

~3.92

-4.90 ,

-5.89

. -:7.84

-9.80

-li.75 i'

. -13~70

"'-

t'----: -TABLE J~- AERODTl'JAMIC CHARACTERISTICS OF WING 6

Aspect Ratio = 3.356 tan & = 3.26 tanm

Cr, On Cm ~ . C.P. e .P • (0/0 Cr ) (0/0 b/2) (;;'::;/---' ~-..

0.275 0.076. 0.0021 '':;11'0.100 - ·66 36 ~

I ~

.231 .055 .0018 .083 66 36

66 36 .190 .039 .0019 1 .068 : I

.151. I .054 ; .027 ' .0013

J

66 36 . I

" • 112 .018 .0005 I ,.041 • 66 36 , .095 ~o15

I

• .034 ·0003 I 66 36 1 .076 .012 .0003 I .028 66 36 I

I ~

.054 .009 -.0001 I .021 . 67 38 !

.036 .007 -.COOl I 1 i

.014 : . ! ..

67 38 ,

.018 .007 • -.0002 .007 68 39 • COl .007 -.0004

I .002.

.001 .006 .002 .0001 ! j . ~

66 -.017 .007 -.0002 1 -.004, 23 I . -.034 .008 -.0001 i -.010' 66 30 -"",

j I . -.054 ,.009 -.0007 t -.018' 65 32 ! [

-.071 .Oll -.0005 1 -.024 66 33 1 v. ...... I

-.090 .014 -.0007 i -.032 66 35 1·· .. ;

-.109 .018 -.COll i -.039 66 36 I ,

I

-.148 .028 -.0012 ! -.052 . 66 35 I . i I ,

-.186 .040 -~0012 ! -.067 66 36 I , I i

-.224 .056 -.0004 ii_.081 • 66 36 . : -.102 -.267 • 075 -.0012 66 38 ..... ---: _-.>'-

L-36P067

L-36P067

a. (deg)

: 17.91

15.92

13.93

·11.95

9.95

7.96

5.97

3.98

3.98

1.99

o

-1.99

-1.99

,-3.98, ..

-3.98

~5.97

~ -9.95

-13.94

-

TABLE'9.- ,AERODTIoorrC CF..t..RACTERISTICS OF WING ,8

-... Cm

0.211· - 0.077 0.0009

• 212 .067 .0044

.184 .052 .0039 /

.155 .040 .0038

.127 .028 .0020

.100 .020 .0023

.070 .013 .0014

.052 • 010 ~ 0016

• 052 .009 .0003

.021 .007 .0006

-.003

-.021

-.021

-.043

-.046'

-.073

-.131

-.181

.007

• 008

.008

.010

.011

• 015

;_J.030

~054

-.oo:n

-.0011 -.0002

.0005·

-.0003

-.0013

-.0032

-.0044

- --

tan e =0.69 tan m

f~-:-·":---~--·:

[ 0.092 : ; . ~

,j ,

J .055 .

I .063

1 .063

t I .048

I i ::~:. I I .040

I .016

.008 ! ! -.008 I " 1-.008 . I i -.008

,j ! :' i ..... 024 1

! -.008 1 .... i'

1-~040 . , ,1-.056 I,

I '

1-.071 , ~ .. --.- .. -~-.-

C..P. C.P. (0/0 Or) (%b/2)

53

52

52

51

52

51

52

51

53 . 51

49

55

55

53

52

51

51

44

26

35

lW..

39

49

35

79

32

39

39

39

58

18

56

43

40

L-36P067 '-~ < - - ." --- -

a . ·.(deg}

13.64

····11.69

9.75

7.80

7.80

5.8$

~.8.8

3.90

1~95

o o

o

o

-1.95

-3.90

.'

.' -~~G-~~~~~~~~~~"

! TABLE 1ft~- ·AERODYN.ii.1ITC CHARACTERISTICS OF WING; 9 '----- _/ L_:

Aspect Ratio = 2.31

C' L

0.256

.228

.185

.152

o

.147

.109

.092

.072

.033

-.004

-.004

o

-.037

-.075

CD

0.068

.053

.037

.026

.025

.016

.. 013

.010

.005

0005

.005

.005

.005

.006

.010

,"Om

-0.0018

-.001b.

- .. OOll

-.0008

~.OOIO

. -.0005

-.0004

o

-.0003

.! 0 ----.---~-

o

tan .& :: 2.26 tan. m

<;---~.-........... -~

0.098 i·

iC?'! .086 •

~ I .. 071. ~

j

!

.058

.056i

! .043', 1 I

1

I

.035 '.

.029 .

.015 '

.003 .

.003

-.014

-.026

c.p. c.P. (% Cr) (% b/2)

67 38

67 38

67 38

67 38

67

67

67

67

68

68

38

39

39

40

'45

-4087' . -.093 .013

.014

.016

.ooos

.0005

.0608

.0003

.0004

-.033 .

67

67

67

67 .

38

35

36 -4.87

-5.85

-5.85

-7.80

-9~75

-1L69

-1l.69

-13.64

-.096 .

-.ll2

-.111

-.150

-.188

-.224

-.225

-.260

.017

.026

• 039

.054

'.054

.070

.0002

~OO06

.0008 .

.0012

.0012

.0015

-.035 , : -.041 ; ;

1 ': -.043 ! I . 1 -.056

-.071

-.086

-.087

.100

67

67

67

67

67

67

36

36

37

37

----- -----------"----------_._--------- " -----

".. ,

_ ......

"TABlE n- AERODTIL4.1HC CHARAC'l'.h;RISTICS OF rUNG' 10 t .... ____ . ___ / • ~- ._---'

G .

Aspect Ratio 2 .• 29 tan e = 2.24 .. =

tanm '. ~

a CL Cn C-~ C.P. C.P.

(deg) m (% cr ) (%b/2) . i-"---"'::::~'\i

. 13 .. 69 0.254 0.074 0.0034 i 0.098 65 38 (:? I .' .~ 11.74 .219 .057 .0026 : .086 66 39 ,

.184 .042 ~. ~

··.O7~ 65 -9.78 .0022 39 ,-

'.

7.82 .150 .031 .0020 .060 '65 40

_7.82 .155- .031 .0021 ;.058 65 37

5.87 .113 .021 .0016 .• 043 65 38

5.87 .119 .022 .0021 f .046 • 65 39 I

5.87 .115 .022 00019 I 65 ! .

.075 .014 !

.029 65 3.91 .. 0010 39

1.,96 • 035 .010 .. 0003 .015 . 66 43 ~

0 -.001 .009 -.0015 1 0 l i I

0 0 .009 -.0001 I .003 ' ~

0 -.003 .009 -.0003 I 0 j

0 -.005 .009 t

-.0004 0 1.

;-~

..;.1.96 -.037 .011 -.0010 -.015 64 41 ' :

-1.97 -.037 .010 -.COO9 -.013 . 61.~ 35

-3.92' -.076 .915 -.0017 -.029 64 38 ~ .~

- .;..5.87 -.113 .022 -.0020 -.043 : 65 38

. -7.83 -.152 .032 . -.0028 -.060 65 39

-7.83 -.158 .032 -.0031 -.059 65 37

-9.78 -~187 .044 . -.0027 -.073 65 39

-li.73 -.220 .058 -.0025 -.087 66 39

-13-~70 -.256 .076 -.C041 -.100 65 39

L-36P067

~---"--'------".'.

'TABLE 12.- AEROD1'NAMIC CHARACTE..'USTICS OF WING fu' ~"---_/. L'~'

~ 2 , A.spect Ratio = 2.29 -!-an t == 2.24 tan m ,<l CL CD em ~ CePe C.P. (deg) : (% Cr) (% b/2)

i----' .. " 13.65 0.271 0.079 0.0013 10.1001

66 37 f c' 0) I \.:':.51

.087 li.70 , .235 .061: .co14 L 66 37 J

! ,lie 70 .236 .061 .0012

! .086 66 37

9~75 ' .200 .046 .0012 .075 66 37

7.,80, .161 .033 .0010 i .061 66, 37 i 1

5e85, ,

.047' .122 .023 .0Oll ! 66 38 I .040 ; 4.88 .102 .019 ' .DOW 1 66- 39 I i j

3.90 .081 .016 .0009 ! .030 66 37

2.93 .060 .013 .0005 .025 ; 66 42 I

l.95 .041 .011 .0004 1

.017 ~ '! 66 42 ~

.97 .020 .010 .0002 .009 , 66 45

0 .001 .010 .0)03 i 001; j -. ( i ;

-.97 -.018 .011 ,~OOO2 ! -.008 68 ,46 i i

-L95 -.038 .012 -.0002 ! -.015 i 66 40

.,.:" I

-2.93 -.058 .014 -~OOO3 I -.023 66 l~o I i

-3.90 -.078 .016 -.Cf'v05 -.031 66 40

-4.88 -.100 .019 -.0006 -.038 66 38 ~ ",

-5.85 -.118 .023 -.0006 .... 047 66 40

-7.80 -.160 .034 -~0012 -.063 66 39

-9.75 '-.197 ' .047 ' -.0013 -:-.078 66 39

-11.70 -.2.}~ .062 -.0012 -.092 66 39

-li.70 -.230 .080 -.0012 -.092 66 40 i

-13'.65 -.265 .062 -.roll -.106 66 40

.. ~."' "/.-~""

L-C_~_~~-36P067 .. ';~~ .<_, __ "_,. ____ ",_ .', ,~._"_ , ___ :~_._"~ ."" _____ ~~~~~~K~~~~~~~i"~l~~l

.--,--."--- " .. - -.-.- .. -~

'. 0 : TABIE 1~:- AERODYl~J[IC CHPJlACTERISTICS OF wn~G 12 -------- ,

....... -'.

tane ,Aspect Ratio = 2.29 tahm = 2.24

'~,

. :., .. ex CL CD ~ <1, C.P. C.P. (deg) (] (% cr) (% b/?) i·

'0.276 1-... --;-.,

, . 13~58 0.084 -0.0043 r 0.108, 68 39 : -i

11.64 • 239 .• 066 -.0039 !

.093 . 68 38 ·9~70 .. 204 .051 - .. 0029 .082, 68 40 7.76 .165 .037· -.0020 .067, 68 40 5.82 .117, .025 -.0024 .051 : 69 43 '4.85 .097 .021 -.0019

.~ ~

.043 69 44 3.88 .076 .017 -.0017 .034. 69 45 2.91 .059 .016 -.0009 .025 68 42 ,

i-

1.96 .039 .014 . -.0006 .017 68 43 .97 .019 .013 -.0003 .008 68 42

r 0 -.003 .013 0 10

-.97 -.025 .012 -.oo:n -.006 . 64 23 -1.95 -.044 .013 r-.OOO4 -.013 66 29

-";

-2.91 ~.o66 .016 -.,0001 -.021 67 32

". .. -

.' L·36P067 . __ ~. __ . __ ~_~. ~_~_~ S{~~~1*~~~~r~~~~~1s~~~@i~ _~~ __ ~. _, __ ..• ".c. ___ • _. __ :-~ •• _ .

-

.-- S-~~;g;h~~~~65JEi~~ ,:

.-'-'-"'--- '-. - .. ---. , TABLEllt.- AERODYNPJilC CH.llliACTERISTICS OF WING' 13' .------ !~:

,. : tane . Aspect Ratio = 2.27 = 2.22 . tan m

a'; ~ C .

Om' .~ c.p. C .. P .. (deg) D

(0/0 cr) (?/o b/2) r--'--~-"~':

-13.79 0.253 0.069 -0.0019 i 0.091 , 67 36 " •. ~I ,

11.82 .222 .054 -.0009 . t

.080 67 36 !

11.82 .221 .054 -.0013 .082 67 37

9.85 .189 .04l .0001 .072 67 38

7.89 .152 .029 .0006 .059 66 38

5 .. 92 .113 .018 .0004 .044 66 39

4.93 .095 .014 .0002 .036 66 37

3.94 .075 .011 .0003 " .031 66 41 2.96 .054 .009 -.0001 .q26 67 47

--:1.97

r . .015 .036 .007 0 t 67 43 , L. __ ..

.99 .018 .007 -.0001 .009 67 48 i ". I

0 0 .006 '-.0002 I ! 0_ I

0 .004 .006 .0002 ! .002 j I

- .. 99 -.016 .007 "

-.0003 }-.002 64 II

-1.98 -.034 .008 -.0004 ! -.012 66 35 l

-2.96 " -.052 .009 -.0005 i -.017 66 32

-3.95 -.074 .011 7 -.0007 1-.024 66 32 -

... 4.93 -.093 .015 -.0009 -.032 66 34

-5.92 -.111 .018 -.0008 -.43 66 38

-7.89 -.149 .027 -.0010 -.056 66 37

-9.86 -.184 .040 -.0007 -.071 66 38

-li.8] -.218 .05h -.CC02 -.089 67 40 -ll.83 -.216 .053 -.0002 -.083 67 38 -13.81 -.250 67 38

L-36P067

. . ---- -- _ .

, TABLE 1$.- AERODYNAMIC CHARACTEFtISTICS .oF WING 14 --"---~-~.-- '-...-.- '........--._---

'I"'. Aspect Ratio = 3.055 tan e = 3.27 tan m a CL On .Cm Cb' C.P. C.P.

(deg) (% or) (% b/2)

13.7.0 .0.272 0.073 0.0.019 ---.....---

! .0.100 66 31 i .. ," \ { 1l.76 .23.0 .054 .002.0 ~ .~' .083 ' 66' 36 -.

f ....

i

11.76 .231 • .055 .0021 ! .084 ; 66 36 j : . ;

"

9.8.0 .191 • .039 .0019 I • .070 ' 66 36 ;

i

7.84 .150 • .026 .'0014 .054 66 36 !'

5.88 .112 • .018 .0009 • .ohl 66 37

4.9.0 • 093 • .014 • .0007· • .033 . 66 35 J

3:92 ~.o75 • .011 .0006 i • .028 66 38 1

\ 2.94 .055 .009 .0006 • .021 ' 66 37

1,,96 .037 .CXJ7 .0004 • .014 66 38

.98 .018 .006 .0003 .007 65 40

.a • COL • .006 .0001 .0 :-~- "- ~r""'-:---·-;..

.0 .003 .006 i. ,.0 I ~ • .0.01 f _____ -:. _ ..... _~ _~ __ .:

-.98 - • .016 • .006 -.0002 ~.006 65 36

-1.97, - • .033 .007 -.0005 - • .012 65 35 i ,

-2~95 - • .053 .CXJ9 -.0008 I i

~ - • .019 65 36

-3.92 :-.074 • .011 -.0.0.07 i - • .026 66 35

L; ~.

-4.91 -.093 • .014 -.COl1 - • .034 66 36

-5.89 -.112 • .018 -.0013 - • .042 66 37

-7.85 -.150 .028 -.0019 - • .056 66 37

-9.81 -.187 • .04.0 -.0021 - • .07.0 66 37

-11. 76 -.226 .056 -.C021 ;

- • .088 66 38

-11. 76 -.228 • .056 -.0025 ' - • .087 66 38

-13.71 66 40

L-36P067 S;ft;~1;~~f~~f0}~@.J)[~~5 . . -. ---- .. -~ ~~-.~ --"

, .. --.... __ ." ~ ... . ' < •

.--~~~~~~~~1J~

/.

·c :-T~Bri~~~: ~ AERODYNAlfiC CILl\R.4,CTERISTICS OF vaNG:15

Aspect Ratio = 4.0 tan & = 3.88 tanm

a C1 CD Cm ~ C.P. C.P. (deg) (% cr) (% b,(2)

13.68 . 0.271 0.071 0.0044 65 35

11. 73 .230 .052 .0039 .079 65 34 "

9.78 .188 .038 ."0'032 .066 65 35

7.83 . .148 .026 .0024 .052 65 35

, 5.87 .112 .018 · •. 0018 .038· 65 34

h.89 .092 .013 00013 .033; 65 36

3.91 .074 .010 .0011· .027 65 36

2.94 ~055 .008 .0008 .019' 65 34

1.96 .037 .006 .0006 .012 65 33

.. 98 .... .019 .005 .0004 .006 64 33 .-------.

0 -.001 .005 1 .-_

fa: 0 ~-.-~- -:----- .~ .. --.-.'"" ...

0 0 .005 0 . .001· .

-.98 -.019 .006' -'.0003 -.006 65 30

-1.96 -.036 .007 -.0005 -.012, 65 32

-2.94 ,-.054 .009 -.0011. -.019 65 34 ,

[--.025. !.:!".--

-3.92 -.072 .011 -.0011 65 3.5 \

-4.89 -.090 .013 -.0011 : - .. 032 65 36

-5.87 -.109 .017 -.0015 : -.039 .; . 65 35

j

-7.82 -.147 .026 -.0021 ; -.053' 65 36

-9.78 -.186 .039 -.0026 . -.068 65 36

-11.73 -.225 .. .054 -.C031 -.082· 65 36

-13.68 -.267 .073 -.0037 -.~9 65 37 , ,. -'~-_#

L-36P067

; CJ

'.'

"

L !

?

.... 0-", • t· .....

'TJ.BIE 17.- AERODYNPJHC CF .. ERi\CTERISTIGS OF VUNG 16 "~--'--- .. .

..

Aspect Ratio = .1.29 . t.:m 6 = 2.24 tan m

--.~~- .- -- --{.---_. --- -. ~

C.P. « 01 CD em '. (deg) °A;,

~- >.~-i

~...- -'- .•.. -, --.'-"- -.-~.-- --.---.. -.. -.------....... ~ ,- -.. -.-.---,-~-- -,---- _._' ::..:.:'~;' (% b/2)

14.12 0.231 0.068'

12.12·' .203 .052

10.08 .170 .038

10.09 .172 .039

8.b7 .13h ".027

8.06 .131+ .026

6.05 .100 .018

"6 '"'5 • :.J .099 . en8

-4.03 .068 .012

4.04 '. .064 .012

2.02 .034 .008

2.02 .032 r,...,P .............. : -~

0 -.002 • CO 7· .• '

:"'2.02 -.032 .008

-2. ':)2 -.030 _ .003 I

co4.a4 --.066 .012

-4 '1), • \.....'-T- -.Oft .011

-6.06 -.096 .017

-8.07 -,.130 .026

_10 (",0 _ ......... --/ -.165 .037

.... 12.10 -' "107 • --./ i .s·51

-:.!.:.12 _ ,)?C .066 . ---'

L-36P067

0.0088

.0077

.0062

.0069

.0c56

;OC~6

.ccho

~8039

.C·026

.0032

.00103

.C'OlQ

. coca _ r'l,""2t-

0;' -..J '-'

-.0017

- "'134 ." ~

-.0832

-.0051

_ ,""n?'') . '-" -"-"-

-.'J072

-.0'::2)

- . '=l~Jl

.. _-_ .. -_ .. _.-:....... ---~-----.-.:-p--- .. - - -- .

"o:w.f 46 40 ;. r

'.082 ' i I 1 __ !

\ !

.066

I­I 1 .059

I .039 I

.042

f .034 \ I' .036:

.017

.017 [

.009

i -.003

, -.008

-.0.20

-.025.

-.039·

-.050

-.061

-.074

-.082

46

46

46

46

L6

\ /

~.to

42

l>J.!

l,e:' -,/

LIC:: -"

h5

1.6 , / Ltv

~6

I / d.C'!

41

39

--

50

53

28

30

40

Ll

'18

1"7 "" !

38

1/ ..,0

. '-

u····

TABLE 18.-. AERODTIi:-mICCHA.F..ACTERISTICS OF WIl'v"G 17

Aspect "Ratio = h.56 tan & == 1.88 tan m

ct CL CD Cm Ct, C.P. C.P. (deg) (% Or) (% b/2) , 13.61 0.287 0.082 -0.0047 0.092 114 32

1l.66 .253 .063 -.0067 .090 115 35

9.;71 .215 • ole -.0072 .076 116 35

9.71 .221 .050 -.0041 .076 114 34

7.76 .173 .035 -.0070 .064 116 .36

5.82 .1.30 .026 -.0074 .050 llB .38

4~85 .105 .021 -.0079 .044 120 4J.

~.;88 .084 .018 -.0057 ~0.36 119 42

2.91 .065 .• 014 -.0024 .034 116 50

11.94 .047 .012 .OCO.3 .022 112 47 i . 0.97 .022 .Oll -.0001 .010 113 50 I

0 0 ;

.011 0 .008 :·1

0 0 .012 ·0 .002

-.97 -.019 .012 .0027 -.006 127 29

-1.94 -.037· .• 014 .0054 -.014 127 .37

-2.91 -.062 .015 .0043 -.022 119 .35

-.3.88 -.084 .017 .0071 -.0.30 121 .36

-4.85 -.105 .021 .0079 -.036 120 34

-5.B2 -.127 .025 .0100 -.044 120 34

-7.76- -.169 .0.36 .0129 -.066 120 3B

-9.70 -.208 .049 .0l.44 -.080 119 38

-11.65 -.247 .065 .0139 -.094 llB 38

-13.61 -.273 .0Bo .0163 -.106 118 38

L-36P067

.--:

i ~~ ~~.- AE..itODYHPJ;.fJ:C CHAP..ACTERISTICS OF WING i 18

Aspect Ratio = 3.87 . tan & - 2 30 --. -. "&.an m

Cl CL On ~. :':) ~ C.P. C.P; . (deg) " -;~' . (% cr) (% b!2)

----- - - ~---;

13.95 0.340· 0.ll8 . -o~0309 0.127 . 96 36 ,

1i~96 .301 .095 -.0275 .lll 97 36 ..

9.96 .253' .073 -.0226 .095 96 37 r

7.97 .209 .056 -.0184 ;.079 96 36

5.98 .153 .041 -.0135 .057 96 37

4.98 .126 .035 -.0106 .049 96 38

3.99 .101 .031 -.0083 .0.39 96 38

:2.99 .076 .027 -.0065 .032 • 96 hI 1.99 .051 .024 -.0041 .019 96 36

1.00 .025 .02) -.0017 .010 94 40

0 0 .023 .0007 0

-1.00 -.028 .022 .0022 -.005 . 96 18

-1.99 . -.053 .024 .0042 -.017 . 96 32 .. -2.99 -.030 .026 • 6067 -.027 96 33

-3.99 -.105 .030 .0088. -.037 . 96 35 ~ ... -

-4.98 -.130 .035 .Olll -.045 96 34

-.057 :

-5.98 -.155 .041- .0129 96 36

-7.97 -.207 .056 .0178 -.080 96 38

.074 :

-9.97 -.254 .0223 -.101 96 39

-1l.96 -.297 .095 .0262 -.ll9 . 96 39

-13.96 -.340 .118 .0298 -.138. 96 40 .-.------_ .. -

L-36P067

-----_._-_ ..... _------------ ----- - ------- ---- - -- - -------------------------_ .. _--_. __ ._-----_._._---------_. __ . __ ._---

TUNNEL CONDITIONS

Tunnel: LMAL, 9 x 9 inch, M ~ 4 Blowdown Jet.

M 4.07

P 1.3 atm o

Re./inch 1.64 x 106

\

s ~ N .. tt A R .. hl I-S1 E[)2-

fry W~~ lt~