( I ( ... ~ • .,,. • • # ~::. ,·:•;;:(•:·'.'•i• :·;, • . .._. ~ '" .. :/:;' • N.A.E. 'SPINNING' flJDEL SCALE 1/24 Classification cancelled/ changed to: UNCLASSSIFIED By authority of: DRDA 7 /DARFT 5-8 /DAS Eng 6-4-5 D ate : ,._5 ~Ns.:.:o""'v'---"-"'-"'"' Signature: Unit / Rank Secretar CRAD H DRP L. J. Crowe Prepared by ............ -.... "' Approved by J. A. Chamberlin •••••••••••••••• . • Date November 6th, 1953• ··················~···· \ .. - . . Date: Issues G. A. 6/11/53 1 ... . Side Elevation INDEX 'C-105 AIRCRAFT' :. r , " :<,-.. •· ·- • G. A. - -Plan Elevation -. ·:.~ . Aerodynamic Data - Pressure 0 Taps FuselRge _ Canopy - Wing Nacelle Vertical Tail Elevator_s Ailerons Rudder Dive Bra 1<:e s Wing - Nacelle F-i.llet Fin - Fusehge Fillet External _Stores ·, - . .. _. ~._, .. . -·. •. ~~-... -. -;,:;-, •· ' UICI.ASSlflfD I NON cussmt F /Models/15 1- 7- 8- 9- 10- 11- 12- 14- 15- 16- ..: ... 1/,~-· /' .. "'· Y-/ .,e -~ ..Y '/:-:'~:··-,-:, c ·.-- ,,,,s? • c_-~7 :."7·~ c;;_~ --'-:'/,.<~ .5',c: f _;/-/ -/ I I • • ::: . • •;.:f" ·:r-::.~~,..,.~...,, .;. -:··.·,~~.::•-11-•; l • ·' UNClASSlFl£D I NOi Ct.ASS1flt ,, • / --i?- :r C c' ,, . ')~ ~;. . • : -~- ~~ ;~ -, .y -_;;:,.,,-,.;r/':·, 7//,R,/,.::rY /~: ~ ///.'"; ,.e • ..., • • - .., -.: ,."P', - .• -;z*:-:./.tr'~~:·.- :_ • -•c::'::·:-- ·sto r; -':A,/ /A--"~ 2:?t?r# ' ·' ' /:_· .... ::·'·V .. --- ·· .. - . - ,· ,: : -~~-~ .:-~ ,;;_J .:;: r -~~ .~i~ ~~ -~}:: ~-;,,..-E __;;:-,,,,,-,-,,r,-,, .V, V,.,; ,r J .:, -.._ / Y ? r ·.~-·~v ·'~:: • I t -=('::Jo ~we ffd~/ ~; I / ' \ • ,,, "°;. I ,, '~Sc-u - , . • _ _j .. L i .· "I' - .. . A."'? ~--r~c:1',, -- L .. __ .,,.,,,.. ..- ••~-- d ~ i / ; · I I / / , . I , 1' - ✓ I I j ., - .,,. I I i / . • . / i-...,- - - - . -- -- 7.-· ......... _ -~;"' ;. /7/✓-,Y,::,j_;L §"/✓~- ~sv,m I NON ctASSmt / I / / \ i ' n ' .,< 6.;;!3'"_ .. ·- ./ J / L / i -,_1 . - "- ·-- _, I ' ·-' ' S,:7/.2,,., - -- - -~r-✓ - ;._~✓-: . · ·- :·,. ('1 - ·• v- ,✓ .,:/ ) ,;-. 6-,f:?':;-?.,.;' ,, ;7-~ / 2'!' ,, ·/,,f:'. .5]t:".,, .... .: ,- I , / . ..:~/ -- ·· 'II ' ,-... • i I ! I i ~ \ ~ ~ ~ .f 1:~.:·' S:~ :• · .-~,_ .. ::xi _:<:·.:--_.·! r.r' : '.':: " · _,.!7/77-.e'".·· 7.:./,2 -~~ .•. r ! ;-:-~.~~ ...... jl !"!~ ~~:). ~~~.ll ,., ~~ . _._, •. :.j,.•:.\ :; :~• ~:~ .. ·~~"; ·•~": ·: ." • .•• · ·/'V,-.),./L-:; j;?t'?'7 ~ C: / t: 5 "41 .ir c-.l'f' .4 ,..,,- r . . • .. f'. •.• .. ..... . _ .. l . :.·· ,, ...... ~,~ ·.-s-1"..,. ~ ... ~ _,.- .. ,,_..1>c ' _,-:!'-;-r,A.-7 . -:..-·-~--- .,.--:,,.,..i: ·:.-~ .. ,. -:r;:,.· ..... ~ .. -~~_,..,-_;.;,.,;':~;,;,,:, .. ,1,,. -~~ :;/- ✓- L:~✓--✓•~; c.~>·~,. ,,. 6.,,f?-~.";.;- ...,.-:"_,;.,.c~✓. .:.: ~.:-~-·c·r~-Z7 ( ... / OICLASStrtED / NON cwsmt· • ' . . y.. • '/I,-.;,-:. ~· ·~ . ' ,_ .,.-..,,-E #' ,.,.v ,<; / /V-=,_ , t:' '·'-,rs /:f c-'7 ,.M?~ . ._--7,/ 4,,,;;'? .. . _g y..,r~ 7/1/54 .• - ,.. ..... _, •• •••• -;.- '"i,if:Yr :.----..:· ,:~:_ -•!:'-· .. r-:-. 5,-": · .. ·-. ,- .-·.,•- ,.··r-.. ··· -r; --:..... ·: C Date: F/M~d~ls/15 7-1-1 r . Issue: 2 , Viil~G DATA UNClAS~irtm I riON ClASSlfll • ~ 'C-105 AffiCP.AFl'' ( <;HORD PLANE DATA ·· r"'" !AIN WING I -•; : N0. DESrRIPI'ION '!'RIG. FIDJCTI0N COORDmATE DATA RnOT T/JC'IllT 1 leading Edge Cot.an .54"3 ,;42~9 y 0.00 6.~92 ··,r 61° 23 1 3~3.29" Sjn .".779 3258 yw o.oo 12.637 Cos .47~ ~42~ Zw o.oo o.oo. 2 Front Spar Coten .6045 41278 X , o.oo 6.~92 w 58° 50' 43. JO" Sin .3557 7362 Y,, 2.527 13 .927 Cos • t:;~73 5046 Z,r o.oo o.oo 4. Main Spar Tan .6~64 717c:iJ Xw o.oo 6.1392 '34° 28' 6.5911 Cos .s244 3757 Yw 10.958 15.689 Sin .5659 5300 z.., o.oo o.oo 5-A Centre Spar 1 Fwd' Tan •• 5235 36245 .~ Xw o.oo 6.392 Cos .8859 0522 Yw lJ.545 17.153 Sin .4>38 66.Z8 Zw o.oo o.oo 5-a . Centre Spar 'Aft' Tan .J606 00783 Xw o.oo ·6.392 • ( Cos .9407 0715 Yw lb.lJl 18.616 Sin .3388 OJI/J Zw o.oo o.oo 6 Rear Spar Parallel to x" o.oo 7.518 B trailing edge Y..,, 18. 717 20.204 B z. o.oo o.oo 7 Elevator Hinge n n Xw o.oo 7. 518 B A y 19_g75 2J .361 B . z: o.oo o.oo 8 TraiJ 1ng Edge Tan .]976 65122 ~ o.oo 7.518 B 11° 101 52.51" r.os .O\}JQ 1865 Yw 22.500 23.()86 B Sin .1q39 1316 z..,, 0.10 o.oo YEY Angles represent sweep A This T/E vaiue (2. 625 11 ) constant to x..,, = 7.518" (elevator tip) B These values taken at eJevator tir (Directrix•~) X,, Sranwise value Yw Chordwise value Zw Vertical value ·,. ... UMCWSlfl£D I NON CI.ASSIFlt .. . ~ .. Date J . 6/11/53 . . ___ ·,-; • . • Issue , i. • • 1 • , • • • ~: .• ·: P /Models/15 • _7-1~13 . .• • . -1. ' . . ! • WING DATA . ·..,. "C•l05 AlRCRAFT .... . ' • DIBECTRIX t A-f , . ~'CODE F/S R/S (1) (2) (3) o.oo 0.024 0.138 0.415 0.692 1.108 1.521 2.100 2.383 2.988 3.594 4.200 4.805 5.411 6.017 6.622 7.228 7.833 8.2Z'{ 8.829 9-538 10.600 10.~54 11.525 12.017 12.725· 13.433 14.142 • 14.822 15 .980 15.980 18.605 (1) Elevator Spar ZR UPR. o.oo 0.029 0.065 00098 0.116 · - • 0.130 • · . ~, .>. -0 .111 ·- -;:• • :· • .. --' ·" '_;\o·.143 • ..,,_. • • . '~. ' 0.144 • 0.11;6 .. '· .. 0.146 • 0.145 0.144 · O.l4'.3 ·· 0.141 0.138 Ool'.35 0.131 . 0.127 0.122 0.115 0.104 0.100 0.094· 0.089 0.081 0.074 o.o66 0.059 0.047 0.019 (2) Mean lin8 location ZR LV,'Ro o.oo 0.033 • O .079 0.137 0.178 0.225 . 0.263 0.305 o.~2 0.,53 0. 'J18 0.'f:6 0.4~ 0.417 0.419 0.417 0.412 0.404 0.398 0.)85 0.366 0.331. ., 0.318 0.296 o.'.'f? 0.249 0.221 0.193 0.167 0.121 0 .O.'J'{ 0.019 (3) Trailing edee depth taken normal to mean line R/S to 3 flat plane area . f .. : .· . .... • v,."·.. '··•·:•~;.'. ~- -~--~~ .. ·:;,--~•.-.~ ~rR.W_ ' . ~ :,,~ -~~-· -- Date: · : 6/11/51 _.' : -- ·P/Models/15 __ ,· :· • • • 7-1-014 • • :.: • • Issue, • .. 1 F/S n/s (1) (2) ( 3) (1) (2) ( 3) /;'' - ' :;_ .., : -. .... -~~- •• • ' WING DATA· . ·. o.oo ·, •• 0.01, . •••• 0.078 ·, _. 0.231 • 0.388 0.621 ~ o.s54 , ·t~l78 _:-,1.231 , __ , __ "-l.'.345 :'; •• .. 1.;459 ; 1.574 · 1.688 • 1.802 1.916 2.0,1 • 2.145 2.259 2.333 2.706 ~-145 3.583 4.022 4. 'f/5 4.680 5.1o6 5.557 .5 .996 6.417 7.575 7.575 10.200 _. •:,. :', j:g:~t ;;f\/L_ ~:--\-)_g:i~ . - . ,._;,)0.078 ., .. ,,. . . . 0.176 • ,·· . .- .i • -.:::l o· . fVffl • • ; ., . . • o 18'1 • .,. ~ ; _ . ·., ev 17 ... :..,._• • _.·· _ -- • ;, , ,,.,: :- -'.":,-0eCf'l9 • ,-.: • • 0.189 _-.~::o.oso ·•· · 0.194 :~. o.oso · ')" 0.199 0.080 0.204 0 .080 ·, • 0.208 . 0.080 • 0.211 o.oao 0.215 :· : o.oso 0.216 . 0.080 0.225 •• '.o .rrr9 -o .229 :· o.078 \ 0.229 0.076 0.227 · ·,. 0.075 · 0.223 0.073 _ ().218 0.071 0.209 o.068 0.197 0.063 0.183 0.059 0.167 0.047 . 0.019 ' 0.121 0.017 0.019 ' . Ele,,ator spar Mean line location Trailing edge depth taken normal to mean line R/S to~ flat plane area ·- , .. -. , . _:.•-~~.;>:~•;"£ir:.,. £-~ ?•:!° •~;_ •-~-- ~~L 1 ;_ -:.;,._, .. __ ,, . :·~:_:-~ .,•~~,r ':"•~"· ,:-· ... ::-_•· -~FD-l°D"'~rit -:. ~ -· ;· -'-T ·:_ , . P/Models/15 7-1-015 . Dates 6/11/5 3 Issue: - 1 -, '.',:-:,r - • ·0.017 • 1-r, ,--0 • • 0 .or, ,, 0.018 . •. . -~ ... , 0.018 .. 0.018 0.018 0.018 0.018 0.018 0.018 0.018 0.018 0.018 0.017 I .0.017 0.017 ·0.017 0.017 0.016 0.016 0.016 0.015 0.008 o;oo. 0.006 0~013 0.019 0.026 ·: 0.0:33 • o.o~ -o .0'.38 - 0.041 0.044 0.046 0.047 0.047 0.048 .0.048 0.047 0.047 0.047 0.046 0.045 0.045 0.044 0.042 0.041 0.040 0.018 0.0;6 0.035 0.010 0.008 - (14) Aileron spar ,J. point of tangency (o/w flat plane) (2) Mean line location (1) Trailing edge depth taken normal to mean line (14) to (~) flat plane area ,r .. .. .... . ~:\~~~~- r-~; ::· .. ·. .. • - . : .... ·.::- -::._ - ·/3 - - ... ··<"('.:/:'.i: ,;; - - ' •i. -~_\ ·. i ) WING DATA t C-105 P.IRCRAFT 1 • ·DESCRIPTION .,,, - . - . The profile of the •w:t'ng1 and 'verti~al tail' do ·. not follow the usuRl conical pattern hav:i!lf the leadinr, snd traiHng edge a generator of a single ··cone. Wing percent lines v:ill therefore, not be strairht unl~ s s they coincide with the fener9 trix pat t,ern of the local 'ruled surrace'. The wing vdll con1<.ain 2 se·:rarate compatible groups of' 'ruled surfaces• ter!'llinating at the transport joint. These groups are rener- . ated from a pattern of 3 c.11:"ectrix cur•,res located spanwise at wing . chord stations I A - B fl C'. .This does not imply that the' directrix at station 'B 1 generates a common -profile at the transport joint, ·since the outer wing profile is .generated from second directrix at 'C' • • different in profile to th!=? main _panel directrix at 'A'. "This results ins slight discontinuity at the transport joi~t. ' ' .,, . The · directrix at chord 'C' ( tip) is ·a basic ~.A .c .A •• 0003-63.7 section having its maximum thickness value . (m) at • 365 percent. of the local chord. At chord 'B' the 1m1 value has been fac t ored to .3400 percent of the local chord. At chord 'A' the 'm' ·value has been factored · to .321220 percent of the local chord. The main panel ~xtends from the aircr~ft centre line to the transport joint and is made up of 4 seper,:ite ruled surfaces. The • directrix at chord 'A' i •Bt follow a profile . as shown on sheet 7-1-0J to 011. Ruled section -1-2- will have 'lS outer .i;-eneratcrs the wing • · . leading edge and the front spar. Ruled secUon -2-4- will hRve as outer E'enerstors the front spar and main spar. Ruled section -4-6- ·.vill have as outer generators the main spar and re9r spJCJr. Spars -5- bejng . generators of ruled section -4-6-. Ruled section -6-S- will hsve as • outer generators the rear spar ~nd trailing edge and ui11 be fle.t in profile with a plane angle of 1 25 1 (tan .0248 ~75) about the mean line. The outer pqnel e.xtend.s f.rom the transport joint centre line to the tip and is i'lade up of 2 separ.3te ruled surfaces. The directrix nt chord 'B 1 't 'C' follow a profile as shown on sheet 7-1-03 to 011 i~clusive. Ruled section •1-9- will have as outer generators the wing lea

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