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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}[email protected])[~~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~