lfilK A V R O E C ANADA LIMIT ED MALTON ONTARIO TECHNICAL DEPARTMENT (Aircraft) AIRCRAFT REPO R T N o ___________ _ FILE N O N o O F S HEET S _________ _ TITLE ISSUt: No R £VISION N O REV ISED BY APF'ROV E 0 ev l:lassifitation cancelled / Chnnged to U rJ C~ By authority of ,f1-,/(9 Date % ~-b Signature. .. • • -tJ/3~ ___,,. -............. _ U;,it / Ra11k / Appointment ... fr/ 0 ... ~ ... PREPARED BY C HECKED BY SUPERVISED BY APPROVED BY DATE REMARKS NIIIC: - c:1eT1 AERO/ M.E. LIIRAR'f 87- }2 1 0 BIILIOTHiQUE AfRO I G.M. C:N"'C: - IC:leT DATE DATE DATE CATE A V RO E CANADA LIMITED M .-,LT QJ',,1 - ONTA R IO TECHNICAL DEPARTMENT (Aircraft) 7 L 1-,, .,_ REPORT No ___________ _ SHEET N o AIRCRAFT PREP " RE 0 BY DA T E CH E C KE D BY D AT E CONFIDENTIAL I ..n .. ~vs Ls of +- .i"J G.1 ~t,ructure ov tt:, 'le",noJ ou l i :rforme i farir • ':,n~ :1.10,m ir. .ri,. ::., , 3 .i.na 4. Fi.,.. l s!D,vs tto ovora.ll i. .1.lheJ .tructirs. Fi,;. l r I I r I I A. V ROE CANADA LIMITED REPORT No . ,1~, l MALTON ONTARIO TECHNICAL DEPARTMENT (Aircraft) SHEET No .AIRCRAFT PREPARED BY DATE ~. ~ ', , ,;./ .; p CHECKED BY D ATE ·- - - I 2 ... nc s t u.t the up· ,r ;JOrt -!.on of tc~ .ct,ial fin ,'1..l "lot :.ieer ir.c:..1 ,e 1.r t, 1 ve tr'J.c"" " ... ~, .3e., r . ; . I'.1. * se le tc: "'.JS., ., ction or stres::i in.,.,·, 1 a.'11 , ; redund.mt 'M'1~ 1..de , o r r I I -I z (up) - / / / / 1e2.4•· / 144•· actual fin and rudder Fig.2 / / / Report c. -,h et :\o, Prepare by Date "/05101 ... OJ ,,.1 ,J1,eurly l,,~r/54 Ung Chord .-- 5 - l .,.. 63 - ),G I /' _,,.,.. ~1 -22'7 ,___ -·- ""' .::icale l '' = JU'' t = • moo t = •-'052 Ar= ,150 it.= i..,:S.83 oy= lti,902 h = 1,9058 ---- 1 A5= ;,,443 t 3' ,lil50 Ar"' l.')90 by= 16,818 t = .1900 A= 37'1,'77 h = 1.9105 A - 2..777 8 t = ,1650 ·1r= 1,778 by= 14, >l?4 t "' .1701 A = 335, 8'7 Heport No. 7 510. _.._ . ~av~t N~. ~5 Prepared by· !i., ..;.':.early Date ~ar/54 h = 1. 2846 1,671! ----- --~:= ,_ ·' J'7 t = .2104 Ar= 4. 765 oy= ~LJU t = ,1951 ~= 4,4.W by= 18.%2 t = ,.cl62 A = 51..,2. 56 t = ♦ -008 ,,. = 41!'.?...74 h 2,1541 A J, ) 13 s t = • i75J Ar= J .o/1 .... by= 16. 770 Fig, 4 t = ,1811 t = •-'220 ,,.r= '.i, ,/'l oy= ._4,JJ0 t = • .2064 1,r= 5 .... 74 by= .21-381 h = i,4288 A = .>. (j66 s t = " = t"' .21-<-c A= 61..,.M,2 t "' •. ~000 Ar --150 oy= 18,902 t = • .;;:05~ A = /,.26. 8J h = 1. 9058 t .: . lll50 Ar= l.9Q() by= 16.•'.18 t = ,1900 A= 3?'1.77 h = l.' 1-.,5 t = .IS50 ''r" 1,778 OY= 14,874 t "' ,1 01 A= J_,5,Z/ :~eport lio. '7/<,51L/ .,_ ~n-et N0. ~5 1--repared by ft.!'{.J1ea.rly Date .Jar/54 ---- .,. h = 1.6711 t = .21'.)4 Ar= 4,765 'oy: 21.Jl2 t = ,1951 '\,= 4. ,~_o by= l~.%.:. t = .1753 Ar= j,97~ oy= 16. 770 Fig. 4 t = .2162 A:'.,42.56 t = ·~008 ,. = 4'1!2.74 t = • !31 "= ~ . }J t = .,:.,:20 .ttr= ~ . ..... 71 by= J..0J0 t = • .:064 l,l'= 5,.:.74 C>'Y= -1-381 " = .1269 Ar= '•·"76 1 by= 1 ' . 909 ------ _J--- n = I t : .2352 t = ,.286 , Ar= 6."'"2 A= 68~.76 by= 47.094 t - .2 _c ,,. = 61_:> .... _ t = .19J4 A = 542,77 t = ,2193 , Ar 6,314 by= --4,107 • .2000 '.150 18,902 t = .,:;052 A = 426.SJ h = 1,9058 1850 ,1900 • :"90 t = A = 37'1, '77 6,Sl8 h = LC.1J5 t = .2104 Ar= 4,765 oy= ,(',1.312 Report !,o. '7 /c5101 .i.. Sheet ~0. C5 1-'repared by t,!'l ... fue11rly Date 1nar/54 t = ,216.2 A = 542,56 t = .2220 Ar .J,t>71 by= <-4,030 t = ,,286 A= 689.76 h = ... 1488 h = ,:;.4229 t = A= of= .1951 4. :!,-0 t = •h008 lf'.% .. ,. = 4t,:,. 7:.+ t = ~~r== C>y= A=4,870 s .~064 5._74 .21.J81 • ----------,.. ;: 3. 1, s Fig, 4 t == ,1869 hr= 4,"76 I OY= 1 • 909 t = .2l.d3 ,.. = Sl.>,,.,2 t = .1q34 A= 51,L ..,7 h.r= 1.500 'J* l\.r= 7,516 l.r= 116 h = 2,1249 t = ,2352 Ar 6,"72 ~ye: .:.7.094 t = ,2.42 A= 411.~8 h = ,2.7~18 As= 5, -:;~5 t ::, ,2193 Ar-; 6.314 by= --4,107 • t = .1°99 .i..r= 5.761 o:;= 21.320 t "' ,..265 A= 779. 68 t = • ;:0'7.3 A= 689.55 t t At oy, ------ ------ 't..51("1 . l5 ,t. !'i.J~ear .ly hlar/54 = ,.~·71 , ,.4.0J0 .1869 4_.'776 18.909 t = • .c:286 A= 689.76 t = .1934 A= 542,77 '1 = 2.1249 t = .2352 I Ar-= 6.'7 .... 2 t "' .. ;,/42 A= 411./},8 1 by= .:.7.094 l I - As= 5.2..:5 1 h _":_ ~• 7)18 t = .219) Ar: 6,314 oy-= ....4.107 t "' . :..265 A = 779.68 t = ,2500 I I l I I t = • .,JJ7 y 7,591 by= ,:,r1.un hr= 2.1.75 Af= 7,998 lr= 116 ---- ----- -- ---- As= 5.744 n = J,0c77 }· t = • .2,',JO A= 877.ll. I ,_ h As t Ar YZ-Yl = A hr Ar lr t t = ,2500 I 0802 989 t = •..:.41 A---= 46l.2l ~7 I ------1 t = .... ~30 A = 877 .2.2. t- = .25w I I I t = .Z313 h Code ~ half srur height = spar tu-ea "'panel thickness Ar = rib area 7_;:_-yl "' oy = rib length (spar to sp1:1r) A ., panel area hr "' half foundation beam height Ar '= foundation beam flange area 1 r = foundation bea~ len~ hf= J.600 a-r- 9. 01i; l_r= 116 Ar= c.478 t = ._406 (in) (iri!) (in) (inZ) (b) (inZ) (in) (~) (in) 6y:: ~7 . 105 A= 5~4.16 I t = . 2.500 _ .L = ,.,,509 { h.t-= 4.9,25 .._ ii.[= 9. 558 lr= ll6 1-..5 = 3 ,0<;•9 A V. ROE CANADA LIMITED MALTON • ONTARIO 7/0510/1 REPORT No ___________ _ TECHNICAL DEPARTMENT (Aircraft) SHEET No. u7 AIRCRAFT PREPARED BY DATE CHECKED. BY D ATE ,Jet.nod The "valuation of t.,e four b;;.sic "nutrice.,: influe!'c"" :ntr1.x:, Cik; redundant stress 'ld.';rix, K. ; statically deterrninant ~tres loud 1J.trix, lp 0 ~ s~ and loJ.d at the point a for the loading ca,se ;;, "latrix, ·-l is tho only J a .nanuul c"lr-n ... tatirm necessary, for o:-ice tnese matrices ure illON'1 t:in ~e ~:1in- der of the co:r.;:...1tati0n co.n be carried out by the I. 3. Electronic vornputor, The follo?Jing is a brief description o" th1::: necess~r ... mua.L co:rrputJ.tion. a.) For r i ; i..1 found-t ion be..: is 1'ae sle:nents of the Cik :n.:i.tri>: (i, " == 1 to 5 ... incL) ure co:nputed fro:J •,he ;,.sJu"led pn:•.sic,;.l propertic-s by t.1e follo.v::.n, fornuL.e fr0:,, .l.Bport Jen/1~1 C, jJO pp. 10, 11 and 08 r~sp .. A (, - X ) "- V s .. ... 1 ll + j (x, - "'i) .x,,J c- ., 11, 6E cos~ I:, A lC - 1) -t i:;;n c.-;.,. 6""n1 -i 6E cos,0 s \1 (x" - ''!) 2 3 (x, - ) ' ~ 6" + --Ll - xl /4Xl' rJ. 6E cost 5 ,:. V V [l ' A V. RO E C A N A D A L I M I T E D MALTON • ONTARIO TECHNICAL DEPARTMENT (Aircraft) AIRCRAFT for ,ul 0 n -+ 17 = y 1 ncos c s r 7/051(.:/ .L REPORT No ___________ _ SHEET NO PREPARED BY DATE CHECKED BY DATE l to .,. ir,cl.. ) ._y t ... e fcllodt res .. T CO"tl C'JSJ _ ie1x~ ... .:n(!.'- - Jb1 ) r . ele en+,., :>f t'l, .., -l;rix i, K = l t0 ;.., .;.ncl.) .:.re co ,pu",cport Je 10 , 'l ,o r _ < ,., , :licti fter ci!1h":lat, i.on y iell.ls Jy tl.e ,ell :moJl'll J ... tho rorraula Hence 1: m ,.. 1 1' l I 4 r, ~ an<1 t ii. L, T ....... t ... vell as AIRCRAFT A . V. ROE CANADA L I MITED MALTON . O N TARIO TECHNICAL DEPARTMENT (Aircraft) 0 nL SHEET No PREPARED BY CHECKED B Y ..:e ii,:;. 7 .,Je Fig. c, add.Ltioral Plc'rt" ts in • Le c1,<: n.,.tr x to .. c.count for tr,~ tn.ln "·" rry c ! t.1':lSe be- 1S • A., ~ r sul .... !.t is neces::; 'r:' to incluJa .J..so the c0rT~ spondin • 0 ele,•cnts ir, tne T ;,nd s. "?latric,,s. rno a. 'itior,al ele.r•e.c.tJ for t!1e (, ii<: ,\..1,... ., 1:.. "ip :nc1trices ( i,-;: located '!lo:'lent. V By t.n ordir, ... try ')c.:din" + ,ieory ·'t:11 ~ 6r ~ = 4 "r1~f 4-h,.l..,. • J. DATE DATE A. V. ROE CANADA LIMITED ~ALTON • ONTARIO TECHNICAL DEPARTMENT (Aircraft) REPORT No. ___ : ~, _1,,;~5_1_-.._/_'1 ______ _ SHEET NO il AIRCRAFT. PREPARED BY DATE ... . )_ CHECKED BY b'3&.'1l s+,rese, o,. .. V act on t. ' e ..re , ::.on of t.1e tr iar ,ular ro :it pane :s . .i ince ':,1rn:i, .ir"' se: f ; equilior .. t id .1ro'.lps e ... ch ,;roup cm,.,ists of t;10 e~u,i.:. .. nd '">rp?:.ite monents, one of ti,t- ~ .1c":. 1.n t .:.r.terse ~tion ,f , spr.r anc. t,10 obl.'.. :ue ro, t rib snJ DATE tM ,t.,cr d.C-P,in,; at a flct.!.tious poir,iJ oeymd the root rit. T~a forner •art en intersection ,f _ spar .md tho r :.n t,lis ;: l'in•~. r., F s.r,..l' elA, : .. , rer,resei,t t.1e r .. ctio·i vf t; • f ,' .. 11 i ... ~.:. r be--,:.. . ·,:F 16 cos 4 'r' • -t- . lF ) cos .. -, .. I i IlF .6cos~ &- •J i 1 AIRCRAFT: A . V ROE CANADA LIMITED MALTON - ONTARtO TECHNICAL DEPARTMENT (Aircraft) L Fi,_;. lOc 7/v -lC. l REPORT No. __ .,:__ _______ _ SHEET NO. PREPARED BY CHECKED BY X ., .., r.!F_ 7 DATE DATE AIRCRAFT A. V. ROE CANADA LIMITED MALTON • ONTARIO REPORT No. ___ ?_,_f('_~_;l_O_,_ L _____ _ TECHNICAL DEPARTMENT (Aircraft) SHEET NO. PREPARED BY DATE CHECKED BY DATE 1'u CiK J..e~mt, (i, k =;..,to ',f., irwl.) are not a-x~ct]_ correct di~• -+;o a) u:.c rt ... in+) s to tl.e f ... P,Ct af :-il + • t rlra • ,n bf'J+ e n f'o u.J t ion ',e 1 ., , .r.ic.1 :n =a t .o !.~ec<- ~v' i Jt-n .....r , l ~r ,t.i -:f t,. f"mr,. + io1 °IJea s .. b) inaccur tP. o•ni 1cl-.ine, t,u f )Ur: l tion ~ i.."l y t,1' ;resent re~ult C.il's be...: ..: of a. 0difi 1 tiffne3s. T"1e MJ ifie l st.iffr:"s" is t _J_criL ... ti:-d o~· 0 r, c.dditioru..l eforu"'r.tJ for +,nJ S '1<..itrlx ..ire conputod a:; J.S. ed '.ipar cros:; secti•:m and .., is tne Jel"cteJ fo•v1d.1tion ~ ,a.11 cross 3ection. Tb3 frnmdatioL beam stress can bJ nritten 6r 2- ) . ... f''f 8!ld by .,·J.tstituthl_, w,d = M n t,,e resultin , e,,r ress i0tl f.)r tne f ounJut 'I. :in b<"0..1 - tra.:1s , C'f cru. o four, l AIRCRAFT. A V ROE CANADA LIMITED REPORT No ___ ?__,;--'''--l_J...c;_l _____ _ MALTON 4 ONTAR10 TECHNICAL DEPARTMENT {Aircraft) in ter n3 )f t 1e kn:,wn ~nur ui .... atre.:Js, 5" n .( u Fi,?. 11 SHEET No PREPARED BY CHECKED BY ,( r,ot t .....i:cr. i.."lto co:urutu+ .1.0n r..-ie torsion 1n t.,o r-31..- ce ... l is resolved i.rt,:, co.u_,m,ents DATE ' .r DATE .. "1.d parallel to tne root ri T:ie, le.t~l'lr 1s .,plit, t.t>.lf Ji;,: to tr.'3 roll.I" . spar w-.1 half to t~i, forw&J' • "l . . . ~ l I l,' 5 f. I " I ~I • ~ I ,l l3 44 11 . 58 . , .~t" ....... """''1 .,. 0 - 14. l ' • ap; .. • .t. li 0 f ,,, .. Bol:5 o_:8 l.1,8 1. 1 u .. -:7 ' :i:: . . ,, (- . t:, 1+5 ., . 1 1. 461 l.f-S' 47 o?J !.-' l,.~1. •C, /'i., 5;, I lo 17f ~ l , 9 54 !' ~ 1.., ~J -16.f;' .... I f - .,.. (j ,..,, 'i;i '.o''1 : . . 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I 4,:.., 0 .. ; ,., ~ t., v'' 7 5 ,,.; 4,, "l. i"'.'-,_,, lv 6690 'l 590 1~ 516 .) 54: L.. ~o l; V'9 ... lh 67L 17 ''78 lE 74). .. .. 639 43 .1 ,~5 I ,.2 l.9:.:~ I ~ 1C55 1Ll06 i ncr,;_ I l ., 4 5 (:.. '7 ,.._ 10 11 ' ~- l. 14 ~:;, ;.6 17 18 lq .., .1 ,,, ,.., .!.4 ... 5 .6 ,? ... 8 / )0 }l .... j 34 5 6 l7 40 41 4 4.,, 1.4 4., 46 4? 4 t.,';1 50 51 5 ;3 54 psi UL'' I.,.., 7 l Lj > 1L4 v 1~. "'4 u-o L.. 'j .x,5 L•J 1,, 116!. l)lS4 .. 1 .7f-5 ::.E. '4 : LL. .::.,.,CJ .451-11 - b38 ,_ J.4.. '1 .1 ::._;F 6 4t>48 :?.u 3040 4050..'. .761 .. 1580 080 u,.':/6 - s~: .UCf.!.6 C 1,f ff ~I• ,r,q...._ II {iJ g 1 "') 53 1 ,. Sil 1 J 6 ,' 1 ~ j I ,.. _. 6 ., b ) 10 11 ~ 1.., l4 1) lA 17 13 19 2J .1 .; ,.4 .5 I 6 I . ,., L. ?/c510 11 REPORT No. _________ _ SHEET No. ___ ....... .__ ______ _ PREPARED BY _. l.r CHECKED B Y I" --.-- -- Fr i lb ir. or r . .;. -- - 4G,c: 1 .v5_, - 4-<,0C .Q501 lCJ48 I . ,04"' 18'79. I .c.,..£,3 .... ,.l/..6. 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ROE CANADA LIMITED MALTON • ONTARI O REPORT No. ___ 7_,_/_'-...:'5;...1_0..,:/_1 _ ____ _ TECHNICAL DEPARTMENT (Aircraft) SHEET NO. l> AIRCRAFT· PREPARED BY CHECKED BY Th'! r·,~.m::;_t,, ...re rreser,teC.: in the for~1 nf t .. ie following matrices: a F rndur.d.mt ~ ... o~ .mt utit lo.d ,nE-trix p s1 final str,3s distri,ution F reduny3J'lt mo:-nents. r' za deflec~ior (rotatibn) t point~ anj tno follo~:L"'lg figures: Fig. 13 .'>ho·:ir:-; for th~ e.pplied 1..:, id Pt:.11-"l s,1et..r stres3 , '.!:, I •I "oun:idtion c-e,;.:n stres, 6' .31>c..rvi1.se· r~xial stres. ,, lj" _1 'i .lib lis,. axi.tl :;tre ;s, II' y ... DATE DATE Fir, 15 snowing t,1e vd.ue along the root rib of tr,e nor.nal 1tr~.,s perpendicular 'to the root rib dl'l..l t he shel.1.1' :,tress r,an r,.ntl.-. l:'t I ~- I· I "' + I I.~ -11 c; i ! I I i -~ ,. I ! . . . I I I ! --L r\.l J ir~- ..... , ,... I I . L -::, -l· · >--4 - -~- I ___ t_ ...J.4_ .,_ I I T f-'-.. :r4--~ - - -- .,., . .J ' f I LI ~ ·• I i ' \l I _J r I h- l . I '. . '--· ---r- - - r --'-r ,., I I '• 1 ~i - r - I t • .. I i '' T • ' I I I _c I 'I""' T ' ' I c---4- 1 -~1- I I -+- - •-i- - - - - rF -+- T I [\1 ' I ·t ,, -' ' ' i \ I I I l . --+·• I I .... , l',, I -t -··- ..... ~.~ -t-- .. T ~is. I ! I I ,- . ...2. -:r· -+- I I I·. I I ""'i_.; • ; ..- · ',. L I - - '·· -+- i 7 ! "----.., . ~ ',. ; --l. -1- - -r· - 'k ~·~1 r .:1 i~ n~ -·t ~-1- ' I • ,, I =· "1 i I I I-. ~-.l_ 1 ~ L- C-J I ' - - - - + - ~-.:._ -- _L_ I ............... I· I-- -- ... - - - I i ' ~ J ' ! I .... t- -l- I I -t--+- ' -- ·--i- I I,. I I I f:, .., ---· ----+- ---,- -- +-- : ~--; . ._ ' I : : I I I _L_ I i-• I --- .,..._- I ---+- -· I - 1- - --t--- !.i.,_ -1 - ·- - . - ' I I I l I I - -r-- I i l- ~-~- I t- .. I ! j i , .• t ... -~---t- .. - f-- - - '-· L:_ ~t- : . -~ I. -r- -1--- ' - ,_ -1- i .. , I I I I ~ . L I ~.I_ I . --+ - 1_ -- - • .-- --~ '- _,.. . f--- I I. • i I I I -- ~ r. j ~~- -i... i I . .~, .. I I 1 . I -~ ' t-.-r-~r- ,_·I - - - i I I I I ' -L i, ! +-.--- r- .. ' - I - - __ j.._ ...... - 1F - I : f.., i I ' I I .. I ,- ~- -4- I -+ ' . ' ~- t ~-~-·-'- - 1---1--- '- --I---- ~ --:: : --,-- . ... -~:!'·"""" rl'..... • i ·-1 ~·· '""' I I - .- · ' I ,. _,_ - - -- ,____ +- ,__ - '---. ' -- I ..1J- , ....... I • I ., . I -- I +..-~ .. - ~. .jr" - . ~------ '- f . ?i~ J.i. l f.. . :.. ' ' r - . t. + . -- -•- ~-. . . I - ' ' : .. ; \ ,,., l -- - ;:, . - J: . - -- t . . ~ I - l r -- - - ~ t-- f-- ~ ' 1· FOAM 174e i A . V. ROE CAN AD A LIMITED M~LTON • ONTARI O REPORT No __ ,.,..cl_."_:5_1_0.;../_l _____ _ TECHNICAL DEPARTMENT (Aircraft) SHEET No ,J AIRCRAFT: PREPARED BY C A TE R. f. 5. .rl_, CHECKED BY CA TE Note Concerr..ing tne B'>Ul1d9.I"r Co .. dit.i-ms It can ::>e seen fro:1 the ;;,ie. nitriY that a concen+,re.ted 1-,end- ing ,o:nent applied to tne rlate docs no-I; pt'!r.,trate f&r ....n~ is 1ort Li in !i tribution of the no::-mal stress m point , lJ, 2J, . . . due to t11e moment ( ) can be followed. This result of t.he anu.lysis 'Jf tn" present paper ?oints out con~lusively that the represent tion of tne conJitions at the root oy 11eans of unconm,cted foundation b':lans is not accurate ... nd cclll be isl,ading in some cases, The correct method ;,f treuting t.le supporting structure is in ' providing torsion me'llbers b"ltileen oea:ns as ShORll in Fi,,. 16. HO",ever, so:ue J new redundo..nt quantitie,'3 should be' adced in tnis case, as for instance t,m;_ues r i • Hence no exact boundary condition, as explained in report Gerj l0S()/J..,9, shouB be considered tlllless a rnor,; ri~orou.s analysis is extxbu.te bou..'1dar-J conJitions .nay produce even a better rea,1lt th~ t. .• e ex..1.ct one especiw.ly in th•J case where the excct condition is not accompanied by an a.de,p.ie.te tre1:1.tment of' the SUpPort. nowever, the approximate condition is not recommt,nded for indiscriminate use because tne etrain er.orgy of the tor3ion nembers is not uccounted for lr. it. A. V. ROE CANADA LIMITED MALTON • ONTARIO TECHNICAL DEPARTMENT (Aircraft) AIRCRAFT: * For derlv.:..tion see original ~o . ..:put :i.tiow J,.omente supplied by fill bea.ns -« b ,,.,"'\ r-. "'\I"' J' V 'fit , 000 61J , 0CO .... 6 REPORT No. __ ?.;_f._0.:..5...;..l _0'-/ _1 _____ _ SHEET No PREPARED BY CHECKED BY -. ~orsion me::ili~rs u!o·~ents in foundation bewns 'f< 6a:, , o,..,() rigid link ¼0, 000 rransi'erred tor-iue .,,. 41,vOU -91,000 - 47 , 000 - ./' , 0 DATE DATE A. V. ROE CANADA LIMITED MALTON ONTARI O TECHNICAL DEPARTMENT (Aircraft) SHEET No AIRCRAFT: PREPARED BY CHECKED BY A.GrzedzielskL, r.. • .r.3.1ear.cy: 3tress M..lysis of Mult5:-Stur ai:d iilulti-,lib ~ . Ung .:itructures, Parts 1 and ', rr."'c./~ t'90/1.:. 9 ... nd A.Grzdz:!.elski: Unit :.Cad ,._t. od, Gen..'1090, ••I•••••••••••• ............... Geometry D::i.tu C-10'.; A:..rc.rw' ... , F / Geor..., ✓ - • A V ROE CANADA LIMITED M A LT O N O NTAR IO RE PORT NO~· _ __ / ~/ q_~ ~_/ __ _ TECHNICAL DEPARTMENT (Aircraft) S HEET No ___ __,Ac,._ • .__ _ _ __ _ AIRCRAFT· h, TF'uOUC TfON A /30\)( D· 'I__, '~A 1'-•, :::i t!bUJ A Pf'L1£1) L AD:-;. 2. " • 3 • 4 (, PR EP A RED BY CHECKED BY ..:) u. ·- 5 3 2 ,, c: Ii , {J ._ "" TJ, s T,.. 0 u r, o !'I Yv A :i .__J f.:, TI) , , .. c. D ri:: ,., r-,-, i"r"'CZ f>c11Jf. T/v'!UI A,.. MCMO/ ANDUN N,.;. 8c5:;,,:_ /J'i/.f !'o /AJ1-i 1 CN VVA A TTACt. Cµ ::,,{( r < -1 7 5' .. 5.1 Cr l'.tfor._T 1 ,. P /L.>IJt·::, I 1 :'; Jyro,_7u,1ATE .... r t.'IC ._]',. "· · s F (., (Iv' i'->VJ,.;it. :...o,q,,, 6 1),5..,- Rt~u1· ,., ,,/,: (;.. bit)(. /t{ u,- ' 7 ... 6;: P. <,, r. X (,ff R.D WHU<.t. 7,, C C, ... t::i /) 1 -~ 1 :.c 7) , ..... ,,. '3UT LI~{ C' A 1..._ t_lJ., 1 "- C: T),~,f BvT orr IV11 •. WA.,; D O !'< ( 6 " p \.\ , c A t c. y . -r,; ( rt. :. ..) ( , :. 1i R c G J :: ,{ c /'( ..) " c. - A -s. Or< 1 '•l. r H ;) y'{I I U ::::, Ht r -r. D A T E DA T E A. V. ROE CANADA LIMITED MALT O N O NTARI O REPORT No. __ ~7...,../_0_.:-_'_,_..,,_/~/ ___ _ TECHNICAL DEPARTMENT (Aircraft) SHEET NO A-2 AIRCRAFT: PREPARED BY CHECKE D BY -·--1 ,,ft ') i ll.J.: re:, THC I 'HC ,;(«-Al' r'S :F Tt1t:. {UHhtty:, '5p,4, L" J .., ....... tf ~ /< ,i e- ' 'Stit.t.T /J, A -lb J/vl• c. 1t17c::,r.;,_1 re_; So 7,1,,T /l /l1l'(.u,i£,~ wc.,.c :..ut--'/l- -r- ;c7r1tr::.. ,4T 7;;c R e ..) DATE D ATE /rtH{:.":::;c(T•...,t(5 -T!a_,:,r_ YAL.uc, ANL1"- CN .HnTs A-17 AIB UH < l(r_ OF 6' K/) IJ ( T '( Is :::, A· 1:i7 > A·Jo, /iic /J LOA I) ,· h:, Cc.1, ,1. .C: ._ I) ... LU "7CD lcR. /tl(' 7iP ?of... -r-,r.,, OF )I; r F,1-1 ~.i /2.ui;or R ( TIP /o I '':> 6 1 ~II'" Lur-1,),,,G Or Lo1L)$ ~ uc. 7, l o,, Is V:,r r: 01 JHL { .• , :'.I u M t-\ /i 1'.!. '( ,, F :_/MI T Or-a 'Ti;[:. s, (. <-,-ur.c u~ Gr s \.\ t.' - A -3,7 I ~ J ATCD ON \1il', .; ,4 / 'J ') A 33 0 A · J b ,:....! /-1 -:, AT , (.) ~ '> () ! • '- 5 {'Cr ,) ~ C ,.:. 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