P/ !v!ODELS/15 N, I\. . E . SPINNING MODEL C-105 AIRCRAFT I♦ National Research Council Conse1t national de rect1erches Canada Canada C.I.S .T. l. Aeronautical and Meehan i cal Engineering Library J.C . 1.$.1. Bib l ioteque d I aeronaut ique et de genie mecanique Report n0.: ocx AVR0-CFI05- f- /Vlode,{5 - 15 ha s been D down graded to G] de-cla ssified by (Na me) : Michel W. Drapeau (Dept.): A1DND Coo rdinator , Access to Informati on Date : Dec . 7. 1992 • A. V. ROE Ci\NADA LIMITED MALTON, ONTARIO INITIAL PROJECTS OFFICE AIRCRAFT E:'1GINE;i;RING DIVISION N .A.R. 1 SPINNING' LlODEL SCALE 1/24 Classification cancelled / changed to : UNCLASSSIFIED By authority of: DRDA 7/0ARFT 5-8/DAS Eng 6-4-5 Date: 5 Nov S ignature: _ ____i;L,_J,1.j'.LJ:.k::J.:-"'..<'4--------- ll nit / Rank P /Models/15 L. J. Crowe Prepared by • Approved by J. A. Chamberlin November 6th, 195J. Date •••·•••••·••••••••••••• Date: 6/ll/5 3 Issue: 1 • G. A. - Side Elevation G. A. - Plan Elevation Aerod:rnamic Data Pressure Taps Fuselage Canopy • Wing Nacelle Vertical Tail Elevators Ailerons Rudder Dive Bra1 h'lvinp its maximum thickn°ss vi 1 ue (m) ,;t . )65 nercent. of tl-ie local crord . At. chord 'B I t he 1 1 v l 11P :-;,is re,~,... rac' ored ~o . 3400 perce nt of the loc'l l chord . At clord '!I' the ' ;;' ' value Jos.R heen f<>ctored to • ;21220 ~ercent of t he local cl ord . The -nain panel extends fror~ +,he air<'"'• ft centrP linf t,o +'fie trqnsport. joint and is r.i,ade up of 4 seppr••te rc1led surfi1ces. The direc trix at, chord 1A1 t 1B1 follow a profilo as ' 110wn on cs'teet 7-l-:' 3 to 011 . Ruled section - 1- 2- wi l l h~,,,, '3.3 ou",Ei- ,Pner.3+e,s the wi".r lfladinr edge and the front spar . R led secti or -" -4- :iill .,,ive D." outer pene r•itors t1,, e f r on":; spnr and r..a'n ,;f'lr , Ru1e <=ection - 4-6- ,)11 have as outer penerators the main spar and re-ir "P"r • Sp1rs -5 - t'<>~ng renera•.ors o: ru l ed section - 4 -6-. Ruled secti0n -6- .3 - :,ill h'.lve as outer re..,er"" p<1nel e>xtP-?"!C. from tho tra11srort Joint centre Hne to th"> tip and is •11adP up of 2 sc>pr,r te ruleJ n1rf """ . Th i r <>ctrix ,, t, chord 1B1 ,J 1 C1 folJow a profile as shown a•, .,reet ~- 1-CJ t.o C' ll i "lclusi ve . Ruled secti on -1..0- • ill heve a1: ou+o,. ren.erc,ter~ tre ~.•ing lead inE" edge and t.he flat plane ta"'f"P!'lt li nr- . 'T'!oe spar ar r ,r,enent will P·,en coincide with the geriera .ing pat•,ern . Ruled surf ~o -0 -8 - will ha'le as outer p:ener ators the flat phne t· nrent line nd the t r a i ling edre, and being f]at the pene:.:- 1tor1o 3:"" not "P' 1tive to any patt.ern . Since all three SP. ction :,{ \ f I i : l k, "-1 -~ ,, ~ t: t>J ) \\ :--. ~

N.A.E. spinning model scale 1/24 (C-105 aircraft) Report No. P/MODELS/15

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