mPrL'\ll> ^ I NATIONAL ADVISORY COMMITTEE FOR AERONAUTICS WARTIME REPORT ORIGINALLY ISSUED March l^kk as Memorandum Report FORCE TESTS OF A I/5 -SCALE MODEL OF THE TYPE GB-5 COHTROLLABLE GLIDE BOMB By Marvin Pitkin Langlej Memorial Aeronautical Laboratory Langley Field, Va. N AC A ^ WASHINGTON NACA WAP.TIME REPORTS are reprints of papers originally issued to provide rapid distribution of advance research results to an authorized group requiring them for the war effort. They were pre- viously held under a security status but are now unclassified. Some of these reports were not tech- nically edited. All have been reproduced without change in order to expedite general distribution. L - 133 DOCUMENTS DEPARTMENT Digitized by tiie Internet Archive in 2011 witli funding from University of Florida, George A. Smathers Libraries with support from LYRASIS and the Sloan Foundation http://www.archive.org/details/forcetestsof15sc00lang 7// 2^5 !>7 NATTCNAL ADVI'^GPY CC^'MITTEE t^'OR AF.RONAUTICS IvIFKORAyPU^.^ REPOR T for the Army Air Forces, Materiel Conmand FORCE TESTS OF A l/S-SCALE MOD^IL OP T^IE TYPE G3-5 CO-ITROLLaDIE (-LIDE BCI.IB By I.'Iarvin Pitkin INTRODUCTION At the request of the Array Air Forces, Materiel Connand, the NACA i? as'^lsting In the development of a t^'pe 070-5 controllable glide bomb equipped with a "target-seeking" device. Tn order to reea^ure the stability and control characteristics of the borrb in its original condition and with various modifications a l/5-scale model ha? been tested on the fix-component balance in the free-flio-ht tunnel. The terts included the development of suitable means for altering the effective dihedral and the directional stability by simple structural modifications, the development of a device capable of altering the lift-drag ratio of the bomb without changing the angle of attack, and the mieasurement of the rolling- and yawirg-moment charac- teristics of the aileron^. The results of these tests arc presented herein. Force te^ts were made f^r 12 different vertical- tail configurations end the effect of s i:c different sets of wing-tip end plates upon the effective dihedral characteristics of the m.odel was studied. The influence of two sets of spoilers, tv;o sets of double-split rudders, one set of double-split flaps, and five sets of split flaps upon the 15ft-drag characteristics of the m.odel was investigated and the characteristics of the beveled-nose , pla: n-f lap-type ailerons were obtained. Most of the tests were m„ade at an angle of attack of 8'' which corresponded to the launching angle of the full- scale bomb. SYI'fDOI a angle of actack '^f bonb cjnter line, der.rse; v|/ pngle oi yaw, d'-->gre3.s Ct lift coefficient -D /T ±xi u cot^ 1 ^u j.dn.^ 7; ? C-p drag coefficient £q,;2 f Cj, of 0.00030, The results ol firure 15 indicate that the desired specifications for C^ , and C ■, , were met at 6*^ an.rle of attack with these vertical tails and end plates installed. The variation of the latei al-stabllity cxjeracteris tics with an'-le of attack of the model equipped with end plates 6 and V3rtical tails 11 is shown in figure 16. These results indicated that there was cOiisiderable variatlrn of Cn., with anjle of attacV: and that when the specified value of Cn.i, was obtained at 6° angle of attack, the value i^f Cn,i, was too large at the required angle '^f attack of 6'-'. It was further indicated that directional insta- bility would occur at siaaller angles of attack and that, if the vert icr-.l-tail area was further reduced to yield the required degree of directional stability at 3° angle of attack, the bomb would thsn be diractionally unstable over most of the lo'.v angle-of-attack range. It vi/as believed that the variation of C^ with angle of attack of the bomb arose due to wing charac- teristics inasmuch as the results of reference 3 indicated similar variations of 0;;^. with angle of attack for rectangular wings. Additional tests were therefore run to check this ooint. For these tests the characteristics of the model as originally received (tail 1, no end plates) were investigated over the angle- of-attack range. The results of these tests are plotted in figure 17 and are suntuarized with the data of fig- ures 15 f.nd 16 in figure 16. Data for un Isolated rectangular wing, obtained from reference 3, are also shown in figure 18 for purposes of comparison. The results of figure 18 indicate that the increase in directional stability v^rifn increased anrle of attack is independjnt of tail design and, therefore, must be primarily a wing characteristic. It appears, therefore, that the desired degree of directlotiyl stability cannot 8 be achievGd at 8° ani.;le of atta-^.k without result?.]!'? in directional instability at 3n.glea of attack smaller than e°. This concrasion was further substantiated by tests of forvi'ard tails 12 acti.ig together with the original tails 1 - a conf iruration shown in fi';;;ure 6. The static lateral-stability characteristics of the model equlDped with tlie oripilnal vertical tails 1 and forward tails IQ are 'ore seated in figure 19. These data indicate ^hat the directional stability of the model . at 8*^ an^le of attack was just barely stable. The results of figure 19 are suinrmrized in figure 20 and show the same variation of directional stability with angle of attack previously noted. The data indicated that the modal with the coupled tail arrangement would be direc- tionally unstable at angles of attack smaller than 3 . Aileron Tests The data from tests of the aileron sj^'stem shown in figure 6 are presented in figure 21 at various angles of attack for the right aileron alone deflectsd various amounts from 15*^ uo to 15*^ down. Glide -Path Control In order to i;rovide the data necessary to convert pitching moments to elevator deflections required to trim at a given angle of attack, tests were r\an of the model with elevator set at 0°and llO'-'. The results of these tests are yressnted in fi,.-ui-e 22. Spoilers .- Tests were ri;n to determine the effect of the upper-surface spoilers shown in fi'^ure 7, inasmuch as this type of device both decreases lift and increases drag. The results of these tests are shown in figure 25. These data show that although srjoilers of 39 percent of the sppn decreased the L/d ratio at the an'- le of attack corresponding to Cl ~ 0.64 from 7.0 to 2,9 a fxxrther increase in spoiler- s'oan of 22 percent span only decreased the L/P T^atio to 2,3, a value deemed unsatisfactory. In addition, both inboard and outboard spoilers created large divinr moments, parbioula-^ly inboard spoilers 1, and consequently required rather large changes in elevator deflection to maintain constant angle of attack. 9 The large ulvln;); moments enccun'^.ered. with spellers 1 v/ere 'baliGved to be ^jrimarily caused by the influence of the decreased v/ing downwash upon the tail "urfaces iniiTiedlate ly behind . Doub lo-split ru.aders.- Figure 24 pres^^nts the effect of do\.ible -split lud'lers A (mounted on end plates 4 as shown in fif.ure 4) on the aerodyni-uiic characteristics of the model. The data on firure 24 v;sre rearranged In conjunction v,'lth the elevator data flven in figure 22 to show the variation of L/d ratio, Cj^, and elevator angle required to trim v/ith rudder deflection and are thus presented in figure 25, Tliese data are given for the angle of attack 8° at which it was possible to approach the soecified value of lift coefficient of 0.64. The data presented in fi'-ures 24 and 25 indicate that the do\:.ble-cplit rudder A was inadequate as a glide - path control device and would merely alter the L/D ratio from 7,7 to 4.1 for full rudder deflection (±60^). A further attempt v/^is made to lo'.ver the l/d ratio by use of snlit rudders of greater snan than rudders A. The results of tests made with double-snlit rudders B mounted on end plate 3 are shown in figures 26 ;:nd 27, ;i.lthoTagh rudders 3 v:ere tv/ice M".e sys.n ox rudders A, they reduced the L/D ratio only a sli^-ht amount further and conse- qxTsntly no other tests were made utilizing ':he double- split-rudder type cf controls. It is interesting to note that both rudder's A :.rid particularly rudders B increased the lift on the v/ing - thereby emphasizing the critical nature of ali'-flov; conditions aboi'.t thJ v/ing tips. Dc uble-split flaps .- Tests were made of double -split flaps A ext^ridin^; over the outboard 42 percent of the wing span as shown in figure 7. The results of these tests are plotted sirnilarly to those of the rudder tests and are presented in figures 23 i.nd 29. The results presented in flfgare 29 show that the double -split flaps deflected 60^ up end down decreased the L/d ratio from 7.3 to 2.1. This decrease, although considerable, was still not considered sufficient. In addition, a con- siderable change in elevator an-"le v/aa required to trim at a constant angle of attack. L ower-~urface s'.'lit fla^^s .- Figures 20 and 31 show the effect of a Icwer-surface solit flan 1 of 42-.jerc9nt 10 3ps.n locatod as sl'-ovm In .fi;jur3 7. These data show a fairly sir^all variation of L/d ratio ivith dov/nwardly deflected flaps. The data jToin these tests indicated tliat the diving moments caused hy the flaps on the wing were almost wholly nullified en the complete model. This action undouhtedly aroce owing to the effects of the increased wirg, downwash on the pitching inoments contributed by the horizontal tail surfaces. U pper-s\i.rf ace ^^ split flaps . - The tests of lower- surface flaps 1 indicated that upper-surface flaps v;ould be required to alter the L/D rtitio as desired. It was also indicated froin tne&e tests and from the spoiler tests previously discussed that the upwash effects of the u'-^p'er- surf ace flaps unon the iiorizontal tail could be employed to nuD.lify the incremental win," rr.oments caused by flap def'lsctlon. Such conflpurabion would then alter the L/D ratio withoiit changlnjf; the angle of attach or elevator ans-le. In order to determine the proper flaij arrar:.;'em3at and location, tests were first made of split flaps 2 vrhich are identical with flap 1 but are mounted on the up"oer wing, surface over the Inboard 42 percent of the wing span. The results of these tests are presented in figures 32 and 33 ar;d indicate that flaps 2 came ver""^ close to meeting all specifications. Only a sliffht amount oi' elevator tidjustment m^as required to trim and the L/d ratio at 8° angle of attack was reduced from 7,3 to 1.3 for 60*^ flan' deflection. In order to reduce the L/d ratio still further, the s^Dan of flap 2 was increased to 50--percent wing span to form flaps 3. The results of the tests of flap 3 are presented in figures 34 and 35. Although the results presented 'ii these fignros indicated that flap 3 would satisfactorily reduce the L/D ratio to zero as desired, a large increment of up elevator v/as required to trim out tii3 pitching momeiits caused by flap deflection. It appeared likely that the diving moments arising from deflection of flap 5 were caused by downwa.* chcuiges on the horizontal tail such that the tail moments over- balanced the wing stalling moments created by flap deflec- tion. In order to assist In finding the cpanwise loca- tion of a flan, which required no change in elevator settings when deflected, farther tests were run in which flap 3 was m.oved to tlie outboard portion of the wing. The 1-esults of tests m.ade with the flan in this nosltion (flap 4) ars presented in flrures 36 and 37. Thsse results Indicated that •••ith this arran.'^ensnt a lar.^e increment of down elevator won.ld be reqriired to trim out the moments due to flap deflections. A srud77 of the results of the tests of flaps 3 and 4 indicated that a 60-perc3nt span flap located at the center of each wing panel should provide the desired L/d control v/ithout requirint;^ lar,3e elevator changes to maintain a constant anj^^le of attack. The results of such a flap (flap 5) are presented in figures 3£ and 39 and substantiate this belief. These data indicate that it is possible to seci^re a reduc- tion in L/d ratio Virith flap 5 from 7,2 to with only 3° elevator-deflection change beinr-; required to maintain the desired an/rle of attack (8*^) . It appears that even this slirht chan.^<;e of elevator deflection could be eliminated by the e:':pedient of moving flap 5 a slight amount Inboard. CONCLUDING REJMRKS Force tests of a l/5-3cale model of a type GB-5 controllable t'lido bomb in the NACA free-fll:?ht t^ju^j-iel indicated the folloving: 1. The effective-dihedral characteristics of the model v/ere v;idely varied by the addition of vertical end plates butted to the wing tips. Addition of end- plate area bslow the wing sijrface reduced the effective dihedral v.liereas area added above the ^"ing inr>reased the e f f e c t i ve d ihe dr a 1 . 2. The model v/ing characteristics were such as to cause an increase in directional stability with Increased an.:-le of attack. This change in directional stability with angle of attack was independent of vertical-tail design. Consequently, a moderately large a::iount of directional stability- was required at lov; speed to avoid directional instabilltv over speed 'oortion of the speed ranr.:;e . 12 3. Uprier-surface, iip'^ardly deflected, split flaps located at the center of each y;ing ;oanel reduced the lift over drag ratio from 7.2 tc without a:-!preclal:)ly changing the anple of attack (6'^). Lan£-ley Ilemorial A.arcnautical Latoratory, National Advisory Coiumittee for Aeronautics, Lanf^ley Field, Va,, March 27, 1944. Marvin Pitkin, Ae r o nau 1 1 G a 1 j3 nri ne e r . ApDroved: \\ — ^r. ^ ^^ r\ < Hartley a. 'iSoule, Chief of Stability Research Division. R3FER^1jCES 1. Shortal, Josenh A., and Osterhout, Clayton J.: Preli'^inary Stability and Control Tests in the NACA ?ree-?lip-ht Y/ind Tunnel and Ocrroilation v/'th Full-scale Fli^mt Tests. !UCA 111 LIo. PiO, 1941. 2. Shortal, Joseoh A., and Draper, John W.: Free-Fli^ht- Tunnel InvDstigation of the -iiffect of the Fusela.t^^c Length and the Aspect Ratio and 3iae of the Vertical Tail on Lateral Stability and Control. NACa iiRR No. 3D17, 1343. 3. Short>i,.l, Joseph a.: Effsct of Tip Shape and Dihedral on Lateral Ststillty Characteris cics . KACA Reo. "Jo. 548, 1335. FIGURE LEGENDS Fi.o-ur'^ 1 . - Photorraph of a — -?;c"le model of the type GB-5 controllo.ble rlide boTib mounted inverted on the f r e e - f 1 1 rb t t ur.n el b a 1 an c e s t rut . Figure 2.- Three view sketch of the type GB-5 controllable f^lide borb as originally received. All diinensions are in inchep. Figure ■? . - Fhotofrraphs of ~— '-cale model of type GB-S controllable rlide bonb. Figure 4.- Sketches of vertical vinFr-tip end plates tested in the free-flight-tunnel investigation of a ^- scale model jf the type GF-5 controllable glide bo*rb. Plsrure 5.- ^Vetches of aft vertical tail surfaces .. 1 ^' 5 lable glide bomb tested in th.e free-flip-ht tunnel. Liistalled on a -i-^cale model of the type GB-5 control- 5 Firure 5.- "Sketch of forward fins and ailerons tested on a -^-"csle i^odal of the type GB-5 controllable glide bomb in the free-flight tunnel. Firure 7.- ?ketches of glide-path controls tested in tlie free-flight tunnel investigation of a -p- scale m.odel of -' 5 the type G3-5 controllable glide bomb. Figure 7.- Continued. Figure £.- Effect of lov;er- surf ace wing-tip endplates on the static lateral-stability characteristics of a —-scale model of the type G3-5 controllable glide bomb. a = S'^; 5e = Cp = 5f = 5a = 0°. Figure 9.- Fffect of lower- surf ace wing- tin endplates upon the dihedral parameter Ci-i, of a •g--scale model of the type ^'B-5 controllable glide bomb. a = 6^; 5e = 5p = 5a = 5f = 0^. Firure 10.- Effect of urper-sur'^'ace endplates upon the rolling-r.otrent character ": stic s of a i-scale model of the type GB-5 controllable glide bom.b. a = 6'''-'; 5e = 5p ^ 5f = 5a =0^. FTOURE LEGENDS - Continued Figure 1,1.- "Iffect of vortical tall area removed eqiially from the twin vrr-tlcal tailr of a -^-scale n^odel of o the t^'pe GP.-5 controllable glide "bonb. 5e =5a ^'-f ~- '^° ^ a = 8°. Figure 12,- Effect of ren-ovlMP vertical tail area from one o.f two vertical tails of a — scale :rodel of the 5 type GB-5 controlla'ol.e glide 'bo^'ib . a = S*^ ; 5g = 5j^ = 6a = 5-f = 0'""; ri.f:ht vertical tail off. Figure 13.- The in:'^luence of vertical tail location upon the yawinfj-rr.oment characteristics of a —-scale m.odel 5 of the tv^e G-3-5 controllable glide bomb in yaw. Figure 1^:.- Effect of r«^Gucinp; ve"'^tical tail .^ize of a — -^cale nodel of the tvpe GB-5 controllable "lide bomb, a = S'-' ; ^e - 5p = 5a = &f = . Figure 15.- Static lat6ral-c:tability characteristics of a -^-scale model of the type GB-5 controllable glide bomb equipped with lower-surface, wing-tip, endplates 6 and vertical tail deGirn 11, a ~ 6"^ ; 5p = 5p = 5a = 5f = G^. Figure 16.- Effect of angle of attack on the lateral stability characteristic? of a -i-scale model of the 5 type GP-5 controllable glide bom.b equipped with lower- surface, wing-tip endplates 6 and vertical tail design 11. 5^ - t^ - b^ = 5f = 0^. Figure 17.- Effect of anr] e of attack on the rolling and yawing moment characteristics in vaw of a i-scale 5 model of the tvpe G3-5 controllable p-lide bom.b. Vertical tail 1 ; 5e = 6p = 5a " ^f =" C! . Figure IB.- Variation of directional stability with angle of attack of a —-scale riodel of the t:-pe GB-E controllable glide bomb as compeared to that of an isolated rectangiilar v;ing. FJGTnE LT:gj:]vID3 - Continued Figure 19.- llCffect of angle of attack on lateral-stability characteristics of a —-scale mo'iel o'^'' the tvre GB-5 controllable glide bomb equipped with origlnsl vertical tails 1 and forward tails 12. dp = 5x^ = 5e = 5a = 0'^. FijTure 20.- I^ffect of anrle of attack upon the directional stabilltv parameter 0^, of a 4— ?i tjx>e G5-5 controllable glide bomb. stabilltv parameter C^, of a -^-scalc irodel of the Figure 21.- Aileron characteristics of a -^-scale model 5 of the type G3-5 controllable glide borb. ^ = 0° ; t'e = Op = Of = 0*^; Sp = 0'^. c.Ynt..:^r^c churacteristics of a 4-scsle model of the Figure 22.- Effect of elevator deflection on the aero- type GB-o controllable glide borib, dj-. = 5a = 6f = O"; Figure 23.- TZtfec": of spoilers on the aerodynamic charac- teristics of a ~-'-.',ale model of the type GB-5 controllable ?lfde bon.b . 6c = 6-n = Of = 0'^. Figure 24.- ■Effect of double-split rudder? on the aero- dyna'iijcs character! atics of a -^--scale riiOde] of the b type GE-o ccn cro;]la.bie glide bo'-b. Double-split ruc-dcrs A; en'^pj .i.te ^; 6^ -' 6p = £3 ^ C'-' . Fifa-.re 2^^.- ;^ffecc of double-split rudder dof lection? on th? aerodynamic characteristics of a -^-scale model of the type GB-5 control] able glide bomb. Double-split ruid-'i-s A; 5^ ~ '^f " ^°; « - '5^' enUplete 4. Figure 2P.- ILffeot of doubla-spllt ruddcrF- B i.^pon the aerodynamic cnarac ter: s:ics o'^' a 4-^f^&le nodel of the tyoe GB-5 controllable gliae oomb « Oe = o^^ = Of = 0^ ; endplate ?. Figuro 27.- Zffect of double-split rudder deflection on the aerod^iiaTnic characteristics of a — scale rr.odel of the type Gr'-5 controllable glide bomb; double-split rudders 3; endplete 3; 63, = 5f = 0*^; a = B^' . FIGURE L^GH^JDS - Continued Figure 28.- Effect of outboard double-split flaps A SI "1 a 16 upon the aerodynamic charict eristics of a ^—s'. model of the type G3-5 controllable glide bomb bf = .42b; Cf '= .SOc- f^g = 5a = ^r =0°. Figure 29.- Effect of double-Rplit flap deflections on the aerod/namic chara.c teristic'^ of a —-scale niod.el of the tvpe GB-5 controllable glide bomb. Outboard double-split flap A; bf = .42b; Cf = .20c; 6^ = ^r = ^ a = 8° - nO. 3 ^igure cC- Effect of lov-er-si.irface inb-^ard flaps 1 upon the aerodvnajric characteristics of a — scale model of the type GP-5 controDlable glide bo?iu . b^ = .42b; Cf = .20c; C'e - ^a ~ ^r ~ ^'^ • Figure 51.- Effect of flap deflection on aerodynamic fcharacteri sties of a —-scale model of the type GB-5 controllable glide bomb. Lower surface, r.Ad panel, split flap 1; bf> = .42b; c^ = .3Cc; a = 8^: s'a = 5^ = 0°, Figure 52.- Effect of upper- surf ace inboard flaps 2 upon the aerodynam.ic characteristics of a — scale model of the type GB-5 controllable glide bomb, bf = .42b; Cf = .50c; 5e " £a = 5r = 0^. Figure 55.- Effect of flap deflection on the aerodynamic characteristics of a r=-~scale model of the tyoe GB'-5 o controllable glide bomb. Upper surface, inboard split ^r flap 2; b^ = .''i2b; Cf = .50c; 6^ = 6r = ^°; cc = 8° Figure 54.- Effect of upper-surface inboard flaps 5 upon the aerod^^mamilc characteristics of a — -^^cale model of the type GE-5 controllable glide bomb. bf = .6Cb; Cf -■ .5Cc: 5g = 5a = 6p = . Figure 55.- Effect of flap deflection on the aerodynamic characteristics of a ---:3cale model of the type CB-5 controllable glide bomla. Upper surface, inboard split flap 3; bf = .60b; Cf = ,30c; 5a = 6^=0; a = 8°. FIGURE L!jG^^D3 - Concluded Figure 36.- 'Effect of unper- surf ace, outboard flaps 4 upon the aerodynamic charao/^eri s t:.cs of a —-scale Tiodel of the type &B-5 controllable glic'e bonib. Figure 37.- "Effect of flap de.'^lectior. on the aerodynair.ic characteristics of a -g;- scale rrodel of the type G3-5 controllable glide bonb. Upper-surface, outboard split flap 4; 'Of = .50b; Cf = .30c; 5o = 5-, = 0; a = 8°. ■" ' ' Figure 33.- Effect of upper-surface flaps 5 upon the aerodynamic characteristics of a -g— scale model of the type CrB-5 controllable rlide bo;nb. bf = .60b; characteristics of a -5— scale rrodel of the type G3-5 Figure 30.- Effect of flap deflection on the aerodynamic 1 5', contro]lable glide bomb. Upper surface rnid-panel split flap 5; bf = .60b: Cf- = .?0c; 5a = 5^ = 0; a = a^. 0) QJ x: > iJ c o 0) x: -a +j QJ *^ (-1 u o (U > 1— 1 . c 0) •H X) o T3 E (U ♦^ 0) c . --H 3 -f^ cd O 3 o E U CO +J 1 XI CO E 1 in 1 O 0) XJ CJ c 05 d) cd •O .-1 — 1 a. o ^475^ < Sectcrf ^ I -^ ^ i 1 ■7 s ra//-J _J£C ^^ ^ ^ S=z 72?// - 7 JgQ g/* ^^g Ta//-/o fn///)/t7// 1 1 fc 1 MiYrD^M =1 / ? <9 •7 a sector- 7 -7- 7C7//-^ S*Q -^"4 S7/^/e 7t?// ? — = ^-^ •7 ^-=:^ y— 3oci^r s i f //V//7 ^// 1 , t =^ ^^ \ XCf^r^ ^^- ^ ^ ^ ^ ^ t ^P. ± 7 .^*Tf mode/ /ncTJes Double 5p//t flops A Figure 7.- Sketches of glide-path controls tested in the free-flight tunnel investigation of a -^ -scale model of the type GB-5 controllable glide bomb. 5 I-. - 1 D -| t c Flap 2. (up). oer surface) — -^ 1 .'5QC > ^ \ — .4?-f -^ — b ' C oer surface) — / / .30C / f M. fCit' _J 1 b c 1 /7op 4 (upper surface) 1 .30Q C T -.LJII /CII_W y / \ .^oc / f_ ,20f \. ,60^ ^ .20^ Figure 7.- Continued. — ^ \ i \ I ■\. » y '> \^\ / / \ >« /^ i s Vj ■) ^ ' ^ JS I '•'? N >•■< T r" y y '^ ^ > • ' ;■■' h ^ /, y ' :^ 1> ^ % £ / -"^^ * 4 :^ t % • ^ ^ ^ -■I ^ • K, A i^ '' l_-t V \ I 5^^ > / 1 / -:t — \ V i r n^ ?^ r .6 ^f .■3 V ^ \ 1 ! A r -•■i )^ (. \ ^ V ;l ^ \ r- ■^ Ff yi V oi e / It? ^'i s =^. X^ -^ ^ t ( )- — — V A B -C L? CPII — ^ S ^ y |> -/ E ]- — •-^ r vo — r| s < >- — — — -^ «: •-4 v. ,^ ^ K^ V^"* . I \- — — ,1 ' o , J - y-^ ^ y f ^ \\ \ '- -- — V f •C A r'^ - 7 " ,^ ^y v^ "^ — -./ < > y^y ■^ V y 1 ; -tl i \' y i r if y^ \ ^ \ .C / ^ 7 ■ \ 1 ; 'Sv "\ r\ \. ^-"'} - — \ 1 .1 i t / i ■) 1 ^ ^ ) ^^ Jfi , ,/ |7 1 ■ r* >1 ^ ■H 1 "^ iL{ fO ^ "" .o > \ / y r T ^ l} 1 ' ■ \ s ^ y^ y * ^ — .< J y /■ ^nI 1 /■ •5 \^ ^ ^ I."? Ift i^ L, t^ y "'■ '' \ ?■ ^ 17 'ii ^ .L t t \ / i^ ^ A > \^ ■ ..C 'J ■ i — "^ — - f r — """ M k- ^ kd kA m 7 \ d 1^ > !z] — — — — — \ s — — — — r ~~- -^ / ^ 1 1 — — — ^ — ":^^^ < > — ^ r — — — — ==_ s -^ 7~ ^ 1 if -;. ^ c / f ^l-^ ^ ^ A ) ^ ^ ^ V ..c «? "'\ ^ ^ -^ ^ /^ > 1^ i-! ^ <^ V — 1 ^ ,X / \\| ^ r ."J Cf r 1 ^ 1/ 7 ^ ■ r^ \*\ "'t X> 1 [ f X / NAT M .41 3R/ ERO RY -C ^ ^■-'y ^ .oMtdn WUl cs ' It ^y y :-.1 r n C J ".I? — fc6 tl < 1^ 7 A- ■;/ 7/ ''r — (a. ^fif nl ',-h ?/)>//, h^rr ?r 'ri !•'> ^/r <; f'< 7 '/■■ i2 7k 6 •m 2C 1*=/ ^7/ 7 -h< 9 ' ^y< ne ^/ ?-, f Ci ■>// 21 16 Q^ 'K feL J. m Th L j2 o. f r ( /; r ( <■-- -'^ =< r T- 1 "~ ~ ~f 1 ■ I-*'. ^ J • •" ^ <: ^ — -K — X- ^ ->- ' ^ 1 ■^"^^ if- r' > '- 'I ^ .1 — — --- f- "^ m -^ 4 t' i^ — ■^ ^ r- it *■- r\ ,k d KJ c \ |P 4 r ■-"■[ §j \ \ ■ ,-* ^ P \ \ r^ f^ 5^' t« \ ^ > --= r 1 r 1 \ ^^ ^ P /7 7r fl( ■n ./ >( ■^ ■^ / \ m Y>' fiil nr !^ l\ iti / r i < K ^ ^ - 1 rt'^ ■ ■& I rj ^ K s \ r ■} — J ? 7/ °> ft -:;i V. C — s ^ ^ )- — — V s >- ^ — <• — p H — n I hi *-— ^ — — \ \ 1 N — — : i J[ — 4 f£ s. — — — r\* ■- •>v >v "■ s» s, ' yd . 1 •*v ^ ^ V \ J — ~ \ A. N V ^ H -^^ ^ N ,,\ m >?" 1 ^S^ \ J/ % — l£-> vj p r*** ^ ) ■^ ■1 \ (^ \ "->i V ^ v ^N ■~v !^ -4 • J, 1 — ^, ^K > ^ s ^ V jj kS, N . s \ > i ^ U: fi ^^ Cx' 1 \ \ / > C y< \ \ / ^1 — 1 — L ^ / i- /I 3 i^. \ "^ ■^ C 7 ■c t t*ti " i** f^-l if^ .-^ \ ^ Ui n c ^'■ i^^ ar > s S - ' < >L , /^, 4 ^ ^ <■- .sr O p ■■i c n ■ ikl ^ f^l > ■: ? u ^i^ IP - '■ > ^ '' - 1 ■O z. ^ <^ -^ r I MAT ON* 5R/ wsc ERO «¥ ^ ^. ^ ' »M f*in EEP NAtJ KS c^ .Ui ' i h t- — / -/ ? -j ? - •y ( ) • i /) / P / ^ "4 Ali ^jfi r, /- ye ?kV ^v dfc, ?• ; y fi 01 tr A t, i '7 7i^ -ff ( If V°f\ th Ti 1 tr 1 / ( ir *A r^'r T?ij rr "^ V <^ ^ // /* . — — — — 'om "K P -J. /9 ir vcr ta i. 7t 21i sic c It 7,W a /? y> o' ^ r-;? f^ A - rT r ' (0 7 -,] oC z. fl' { ■ i^ :-:_;| I t ; •>: —.r •~ ^. ^ ': ' ■■ ■T_ ^^ "^ • / ^ ■^ r^ ^ 5 ./ ; ■ ^ >; >« C; n \^ " ^ . ^ 4 — 1 — ■fi ¥ ' f ■;'-| — '1 rffl p*^ » Jl tr J te '-[ ^ i d k^^ ^ 3 <^' > f M — ^ ^ ^S T^ g=r Ut ^ ^ n . 1 «j» - - ^3 .1 ri" i " i'.-. : u- '-'I (^ ) ^ - ffl" --_ ---i ^ ■ . . ^ .-^ > ^1 >. -« --,^ -7^ ^ -^ »>" — — > Jl •§ ' ^ -t ^ I " vA SJ A~ __ . -X r "■• -H K< >. ^ r*' >-' \ f 1 q . O" ~ — ■ — . ■ ^' 1^ ^ _ -'S'- - __,, ^L ^-~ ■"' J • -^ i 5 >c -< ^ ^- _ r u ^' "t — - 1-'^ ^ ^-3 ' ^ T i ^ ^ ' — -_ 5 ' -^ ■- s ^7^ V <^ -^ 1- K •V - /^ / > - s fcr ^ > (\t Ii. r7r;V ^ N $ L>f '"iy ^ m Tnd ^ in '/j r ^ ^^ n -> :S — 0- c>ff C\ s \ ^ — — ^5 1 1, z y V .U — — r^-' ;']>- -- 1 6 ^ ffi /? r- -- — U.i V- 7 ^ ^ ; , .'''' -^ '-ir 5d 9 -5 i? ^ ■-■ r > / ■ " : f\> . Q._ J-5 i U ^ "X 'i^A .'4 r r ^ L^ ^ {^ A 1 ^ <> V ^ y< r' "'71 ^ ■r\ ^ [;:V^ <' - --- - ; ■ ^ •> iJi /, '' - ^i i^ 1 V /- /■ -^' ^ ^ \ ':?'' .' " 4? ' '^ i\ 1 5^ / / 1 -: .u. ^ / / M w< f« hnst m \ <> »M Mm ^M DKJ ^RO lAJ cs r / t " 'A s^i L f . : -■^ V' - r ) —< ^ — i ( ) * i / i / p /< ^ i"; 4/ ^'^ //° f V^ L r? n ( If r? '^, ' J ■ t / 7?/ in = / P - ^ =^'"/'^ 'n ^ f ^f ri ^rt r? '//' y* lj ??/ //( T, 1 in, /^ If =?^ ^ >T rr f f ir ^ n, r ^ -y; 'ii r>^' JaL 5£ t i IS ■5o 7 ^ 7 ?V i^ 2^ n f 0^ h ^1 a. 7/^ 2/7 7/ 6U ^ J ?/^ rff / -^Q- y" ' r t 1 -t — ■ " ... - ■ , .,._I , •J ' ^ ) J — 1 ^ ^ ^ . - : f y ^ -^ v^ • <' ^^ ^ ( <" \^K -» ^ s, ■ i . ( V- \-- 1 S /^ X y r ; > .^^ T ( r^ 1^ \ y ; y 'OJ C! 1 L^ r' — f X y' * ,- ^ — f) A >^ — r — — 'i , " 1 — - - f f CJ f .L / ^ ^c x t ~ — — =d -< >- -^ ^ ={, ^ -^ y . —\ y ~? __ „- -— . -; S I' - 1 — — — — — — — — — — -A r =i t. -X L. -t >- — — f=" =t I] — 1 ^ T - §^^ 1 to /• ►/- .£> . /■ )i . jl ' ( ) . - 1 _ -f > — 1 — 1 — 1 ( b^ ^ U- -H J] ?= r< > ^s^ y^ ^ >" ^ ^ T 1 r ^-1 —( T- ni ^ ? ss m ON* . A iVISt RY ^ X>M (im ;ef DR/ EflO uur ICS ^ S t \t I JL h 5_ -/ ? -/ ) _^ i 3 6 ?i ^ i (" i / ? A 5 At)( lit f \/Wi y, !, r? "'i > — --] --; Ff>r}(t M / fj- .^fr? V 'nie, Vf ' ,5?| f7/ y///j f -J 7n 2i r/ V ir) (. "^ ^ 7 m '-^^C 7^ /7?<; -/^ ^/ df t ^ iow< 7/ ^n t?// n' (^) f/<^ ^ /r /7>/) f v/ 'r^ ^ {ah' i — r2 n^ >7 •> J "^ ^ ^ > ' — — ~~1 — — —^ — — — — . — — — — . .^ > ^ y^ ^ — — _.- i> f — — — — — — — — — ■ — ^ C -i ^ -^ — — — ll "o -^ 9 Js '+H 1 ^ ,! 1 5 / "1 H f ; 1 > ) / t^ Y '^ ^ 4 >^ Ti c ^< 7 t V ^ y ( >- ( 1 ^ i ITi ,- ■ - . - — ^ ^ i^ I Y* ■) Z I — « — -. — _ — — — — ~r — — 1 — - — — — — — ' — - / \i — ~ ^ — — — — — — — - — — ■ — — — ' ; — — - K ^ .cJ 7 < >^ ~ ~*" • - -< X. J ■ 'S >- !■< A \ n s . r T .{ 3rl-p i^ V '-i y.-i' 3- ~? ]-^L ]- "~ K __ ^- f^ r t ■) f JJ ^ — Ji i^ i ^. c ) h-^ ' 1 S C J -- — ~ '* ? ^ >' -< >- u_ -< \ 1 1 1 /■ — )/ ^ ■^ ..c '/ - 1 If l r q t 4 i- ri J- -L j^ — . VJ] \1 - -f r -k H< ? ( ) < ) -c ] ^ . f J- - — ' — """ "I ] L J -< \ r: '"~- "-/ S ^ ? ^ ■\ t J t ^-- r r\ > y >^ ^ ^ C I k-> r^ " ' — - -< > S^ -' ^ s < y ^ ^ /> )i -L V "^ u ? Lf' ^ •: t ( ) ^ r - V ? / ?, /, *> f^ W> ff? o/ VA '/If f ('a p^/" y? NAl EE fOR wisbfiY ^ERQNAU CO!) MIT ICS /9^ 7(' 'T? / 5,. L/ y? / r. Ik -,5 a, C6 f fe 2? J4 in 22 «c c a i r ygn - V// ' J/-, 7/?, ^//i y V r?^ 7^ 't/^a, 5;^ T r> id - r 1 '"'1 0;| 7- ad ^1 0^^ ^ 'a <0/;r>, 6_i r; 7r ^ ^/ 0< 2i< ^ j 5_ /k p u > ■1 ^ ^ - / yi y C -■: ./ ft ^i: < J 3^ -^ f o/ !js ^ ^ > ' ^ ^ / ~-^ v^ j\ y :/ / ^ > < \- Js >- — ' "" =< *s < )i .c J <:> — y ' ^< y ^ * V \ is. -^ — &i Y / — — — —f — \- CZ >- — 1 —t V- ~4 U- 7^ i- e -_™ — — K — — — t_ -^ v^ P "1 i ^ I y_ — — — — — V — — — S^ !^ ^ ■■-, < \ 'Jt vy / \' n- ■^ -t T ^ y / ^ / r\ A u< \ J ( ) / // Ui ? > _ — — / y / / $ — r r x- ' y -^ J y ^ d: K'' > X - (\ •S Ui. -' ' |. / ' f ^ y' Li « ^ A 7^ /' [^ ' u 4r o -y ~2 -♦s ni .<■ A r ^ < yJi % A v y ^ / s y ) y j t^ > < r I V — **; — n ■^/ y / y/i -^ ^i \ r "sf 1 ¥ ^ •K ' ^ Y > : tf pi ^ U — u f^ 4 i] - " J" f / ^ V y^ u 1 iNH ONA A wia RY — > ri- ■i \ ^ ?^ ^ > ( ^ COMNin E£fl OR. eroNau ICS Lk Y / / ( ^ ^ r ^ ,^ ( ^ — Or -1 p — ■ '/6 ^ 4 ( ) i f ^ / ? A ' A 0/ •)/f t n f ) /r H f . ^ t n 'P, 7 / Fi Of fr ',9 _ r, r^ rf < D6 ■■ r 11 Mil ai a 11 f pr lot, 2l 9^ 5- '//, / a — T^i '/At/( ■^.'i ^f //■ 1/ fi f. nnP 1/ 1(1° A -^r r\t i ILL ' } 7// *) , r* rh> 70 lb /^ ■> ^H ' n --( y 1 ittRjiJ Mm ' -- 4 si' '. _ -/ ~ ~ h 7 — x:i. f3 \ H- s rk„ ,r r\ ,1. r-^ ■>> ^ ii'^' c i_. ^ V L o ^-^ — — /) I Q )-J- —- ~i ) > — — /<9 \ r ■~^ HT )-.. \ — _ ^ . _ ./^ t . *i "K N > ^ ^ \i . > ) V if ^ , \ \ B r 7 ]^ t 1 t 3- -~, \ \ < > ^ ?s c L 1 \ S-i j^ t>^ :, 's s — \ T-- ^ 1 [1 1 \ tj > y > '-1^ 4 J \, ~ Ih s V \ ^ ri- ^ , --' \ r:*^ f. "A - ; \ fi 1 P 1' _' 1 - - R / »0 I- : iU y ^ . . ri- " - , ' 1 > i ^ , .- I/ I t '" S ^ f/ r 1 -, J n ? 4 f ^V ** / ■ i'-^*- ^ A- c; f-. y A / } i^=l 1 J^ V / f ? ^ / r , / r'- i 5 ^ > < X c n f^ Q i / .1 f-^ -_ N 1 \ \ J \* t^ ji= p^ ' ^ ■^K / *-A r ^~ ^ v t^ ^ / — — (•-■ (0 f ■1 /' . [1/ I / c / ^ - / ' / 1 'ti ^ > /' ■ ./. / iTIO rTEf lAL ADV SOR f / i a fORAEI onAudc » f J^ i " A :i -? ^ rjL 1 I 1 ^ ^ i /; P /■ A 7/( 9 r, f r7 '';f? / ^ / (°, K n, ^/ n 1= ?Vr yi a n 7^ h6 "^J '/?< 7/7 7/c — — 'A If a: n, '\fk:'- (^? a. / M r_^ oo 'el - r 6 1/ 1 c. 3 /?^,1 t 7)1 It i 7/' ^y. 1 _|j __.lJ lii; K:i I'-l' 'T 1 ', Ti !l| ': 1 ''! ■i" ■ ■ ■| L' "i jr; T"''' n-T ItT! -" r— T yi- vv :'l n i"J [ir: .;.'irf, '^'} m s i f- ;i; . ", k f« K • i , , ; I! iji LL < >,>' j^ ■ N ^ * - \ •■ ^il^ \h S ■ ••\ >» 'j-i -i kn-T-T :l C \i & 1 f t J f :!:! A ■". \ ; J'; I- 1-. ^ y ?■ I m* ! i X ' J ■ ,t — — ' 'i't r It:; 1,!: ■ ... ' ll 1 .!J :;,;tTi,i+ittl ^ t / ^^ 4 '.: '■' |-r' 'li p-.i !,■ ;i! l> 1 ■■(■ ,1 -* !;4 J Iff (^ ■ ; ■ t . r **** t?^ tn > 'J; :-ll (. ■^ ,1 '-:■' ' ^'1 :-: J '—. ~ — ? i J?: & T^- ' ' i ' :'-u. : \ * ^■' •■ • y r 1 ' - 1 ■■i S*,: •' ! ' :' ''■' \ / i). ■ '7 f>'^l :i: -.- ^- - - "^ '7 {J J^ — 'm 5r — I H: ^'.; / ^ -- ii! ~ 'i 1 r - <. N 1 ^ f) / ' d ^ X ; iii' !,■ ' ,1; I.. i "■•} '^ 1^ fyfj ■■'~ "" T -- . — I ., 1 ' f f /( > J -^ ) -.^^+4-1-, X / ^ r ' _- , ] / / 1 < \ ' "t. / !■ [:'■-' ^ ^,,; ft 1 % / J " "■ / ' fl ii:. f^ i 1 P . A \ X^ ¥■:■ !';■ : '"■ 4 i::' '■-! \/ % r i& -^^ ^ ■i . : ":■ / ' ^ i 1 :43 }ti^ ^ '•■•}- i -, t I"'. I't! _-M t 1 :.!■ -^*"i / ;tH -!■'-!-■ T C b 1 v.. /' 'fA '• 1 - i.. <^ < > 1 A " -^\ / .<^ S ^ ^ 'm / - V, .t ;;- ijff r - \ ^ . ^ 4 *^ *t-. rv ftxm 5^ r bi i ^ L > ' - 4 !■, i 1 J ^ -C J % ? '^ m r ; ^ » ) , { ) - . - :^ i' ^ ■ -- ^ — -^ ~ a '■J i. ^ ./ ,^ ,i ~- — -^ >- ':i / ^ aJ fjjj f j^ 'i^-^ •^ , ^ - y ^ y- -' 't* r f :;. lUtl N ii_fflffi fimp \y ^ :'l " ,c / ' .y- / ■:|j ."1 1, '' bo Iff rjgtti '"'.'' ^~ c: y\ 1 ^= y / - t) ^ t ?/ _^ ir< i ,_ — — , ,1 c;^ si ' 1 i i y — t':-' ,-^' — \\^ lii *■•; -y- » / ' ^ "K ' 1 — / / ';-; V- r ■ 1, T- ■ ; '■i! ;>:i ^-^ ^ /, ""< «^ ■ • 1 ?■ ^ ft '"i f I '"/! ; I '•v. S' . — -^ -- ,-t -1 i ■ vi ^ -,' ^-j i^T Sa '|. ^c\ ~~ ^ r.S ■^d ^j ' I jp ^ / 1 ''t "^■ S; " .' 1 — — -* i~ cS p; i 1 1 ;■; ■-^ ■s . \ V . :; ] i] ■ ^ *** - ; s \ ■ V f- ■< " \ >: r:l ; ' ■^ ** ■».-• , \^ * : — ~ -- 1 r'-i -/ 9 s s K : '■'■■' \*'- ! . -, '■ . i^-' s !■> -/ s ■, ^ ^ 1 ( 7 • i \ '; '} V /, f, II,: ■ ; ^'' - / ly ?/^ V 11 "Jq r/ \r, " -J V . ^ ^ 1 ■ ^^ ' -, ;,;- < >* f Y - ' ' : ' /; - ' ' ■ -. r v~- — ^^ r > ■ , ? 1 I < >- . - ~ , ._ ^, 5^1 1 "." ^ •.I -■: J i— : ~ -, — M 1^ 1 ; ', . \ -i 7- -r— _- _ jV r'>■ / 4 -,*. ■■t «?? ^ -> -^■' f :' — if.' ■ — "N, \ 1| Y . ^-^ 'j — — — y )- V > _>^ t- *1 ;:--r r.tU 1^ ■;'5 ■ ( } i K"? ^ K 4 !,•' i'l -~ ^J '\ — ~ — ,(! 7 — i k) -T ./ ; >4 V^ ; X' — ^ '^i io $ ^'■ If; .>^ ('i ^-- — — ,,^ '/ ^ ■•f1 *;., ^ vi ■ : ^'^^ ','5 ' f / ^ '/ ":J -i~; ^f !■: ^s* -n ^ i > : ,. // V ' '- t T / ^. ttH 'il p-- fi. % n ■-_- ' ■ ■ pr ; /• / A / : 1 i' •t ' r^ ■-"tJ <; ' ' f / r/ '^ l-* ^y^ \ * /■ & 1 — _ ^ - ') L k^ ^ ^ '"? y ' \ ^ — 1 / ^ I — — :< n "^ ^i ] ■ ' •-N •/■ • r? ~c r r/ r :: — ; 4 ., ' — . \' '-/ ii| /I ) ■ Hfr ;{'• ■J ■ '• i L . .-" u i -.V ■ '~4 ■-'V' ^^l : ■ -^ - ' - - ' ,■ I iii , > '-■? '.'/■ ' . -- ' - , ■■ ' ; i ; i ■ ■ ■"'" f ,,<* 5 ^4 ( ( ? fS i V \ / ^, ■ I'f'- / iy W. I d ^ (7 // fh ■A i '^, n ■"^ f ■ ' -j y" 1 nh ^ fli 7f n f ?-^ '. -/ yA °r, I n r r?!^, J^ '- '?r T <- Y> . ^ i >% "A -y, v , ' ;^T '^3 W \/r f/ V7i 77 '-/ ft A'^\f/< T,^ n^ P. 7 da '-3 V7 rrr 'M /? >n it' / <' f /> *?^. -1 V ^ "'1 U. r n in &< bw7. V( P ^ 6^ 2fe S^ G^ Ki M . ^■5 /?/ '/ A '/C n RT i ■.t (°/ )<7 hl~ 7?* e 4 _ r^l &= ■r^. ■ ! ' - ..;J :_. — - — — . .-, : 1 'l|| Vi i: ■. :,,. ■ ;' ]:\ ,-,[ iiif Is ie m '^^ m n n I'M •s^ ^^ ^ ^ m '?f iS 5?r ?5 *fte|Brtp.f :'rt. ipr ^ ^.^h EH "r^ W n-.l ST "fi 55 'F W pi \4 >. t :- . ;'»-: !■■ i_,7- , > !■■- ;■';{ ■ t>-- C 4 p.-:, T»>r 1 ' i- ; ' , :. — ".I W~ : ■■ -- :■-> I-* ■ ^1 ;* :., ,:: .'1 t J l:"i". ' , ■"-[ ■■'H §-'' ^ "5" r r^ --: ^ ^"! 'i-rt -\m 51: ^^c Jt /.f -- ^rt ;j c 'J ^ > x" f in ;' "■i; v: _j i.-"; ^^r- (f ■< ^_ --' ^ i<' X * ^.-f « ; :""-'T- --, ■^ , 1 - 1 . . t ;.r % )/ i- fV 1° -^ M i ■■ ?' ■ rf ) -r 1 \ 1^ § i — S^ ,\ St'- ■ S': P ■ ir ; -. . V \ -^: — ^^ 1 " ■ ■ 9*" , m^-'' fe; ; .--. "■' !' - ;! fe : ,-1 — — 1--1 . ■) ... f^, » * ^ )° -: 7 <•) — "" r 1 " 1^ ^ ;lti ■■'f P ■ /J J 1 ^ 1^ ?;.■ i-^ ^■f i> . ^•t S "'" f- ? ,;: . ^ ^^ ^ ±- 'f k: , ■"H pfr;> E?- ' / A/ >T^ ■^. ^ ^ pn fc S ' t : ( \ ;--_ -; - - ■s r , p -?■ . E Pt ■A '' i.-!; -^z c o /, h A ] — l^ ^ " ' ^n-r^ ^ — -^' - - : , X ^ -— - vr ! '■'■ ■ r, '', ?if t / . - <:" i . i .;J vv 7 ; ■_. / A 1 -1 , A ihi 1 ? - •- - ^ J , ,. ;!.!; / /;jj >/ ■J\ y u 6. J* *l I?- fe s- i:- t ; -: -1 ■T^, r-H ; /' / fS. r -,- , rf' r". / ' - p: Q __ , — , 1 it '5 ■ L pt^ ;:■; > V ' " -ft J ? •^ .1 f ■'^ t^: / a — ™ w-^ ■^ ' -ri ! s » , " < u U c- ^ h- /' .. ^- (A -^ — — — i Y ft:' • ^ - i* r n 'S i '17 r .^^ ^' <' s> F^ A . _ ■* 4.^ c tr^ "^ ^ — ^k ^ ^ / <" r" V — — .- ■i H ) ■■ 1^ ^' - 5> -^ ? ^. ohr <> s- -< ¥: r 1 r- ' (ATI JNAl AC m ir l^V - - X •> ^ — — u f L ■< lOM uni £f IRA EMI m p, •- ni -' -'' ± /J "- *f H A. J-' Y ^ -r r S2. r _^ I-:- -*. — — '$, ^ -. i- i:; -i f'-' > ■ ■ ■: if i /_, r -I \ - f } I / 5_ , f /i P ■ ffi'^-' T - :-. -^ ^ # ■ t ^ r. ^/( ?C H, 71= ^7 tti : ^ — : _ 1 St "■ :-' -7 p s i --r •' . hj - - ll'" (X-: ^ fil iFi i> ,^ -n - 1 ='/' m ^?^ ^z >i( v/ ^ 9^, y //^ L ,^/ /(^ ^ 9.^ ■f ^, 'if/" n /■/ le ■-■ 'x H nt In -it m ^th ■^s a < -r^ ''/ -r n W 3 n -v a '7 f ■ .""- pS- - i-" tA - ^ - Ik li 0, m ^ '/; rv ^ ? r5 ^f^ a (^> c )". 'r-A jHi p> VI Oi hi a ,? ii 1 > S r -, r ■■ - , ;/'_ :\--l r-j^. - ";r ' ftsfa N /-! +-1 - > La Tfr: Eil a£i u ag ^ 2££ JlL".^ M iii iS it S ±3. iia M M M lli± ^ -*i^ m. 5g M "^P jiigg^ j?/^ ^" M^^. :r+t5 a^^ s^ ■Xt± gsi jE^5^§' Sii' ^; M '&±^. 1- - 4 ^^ :£? i ^'-^^ ■3| * ^^W*fe £4j^ij^±ar^^f^^ ;diJFtt4 ^ \ ^^ "^ r^ m ---) !•-■■ ,i3 '■' • ■ i r>^ ) r 7_ - <' ff ^7 'f^y. ! ^'1 t~ --. ^ ->*. r'i A ^^ V _- !s ^ 1 1 s K - y 4 r I 1 rt R ^ ■ "^ ^ '^ ^ .^ ^-i p , r ; !,? 7 , t ^ 1 "ry "^ X ^ •^ '-^ c •!^ 1 ■) N A \ T rK-- r ': '■^^ f< \t )o i',:-; ^ .^ \ ) ;'.' ^ 'J' ■ l ^ ^ ■ -, 1 > ■1. -'}\ 1, ti ^ ■ , ' ^ ' 1' ^ ' ;• ^ . r ± ^ .« :-a *^ 1 > „ J 1 a\ T U jf]! f^ f > '.[■; — VJ ■\ J Vj ^< ' ^ T= J Yf ■ ^ / 't 3 ^-— •i f,:^ *L- > s, A A i v ■ ' ■ ff{ ^ ~-t /< -o 7- •V •^ ^^ i< Y y. / ./ ih 7 'M v^ ^ J \ < >- ? '/ ■< > . f / < ^ ■ f ''t ,> J V r ^', ^^ ^ J- J ?( \ r J- — — - ^A f — 1 s ■ ^ .« ' "^ ^ )~ -^ ) < >- - - t3\ :7 ■^ / -^ -< i \r- r- - ~- ^4 r ■T'- N , / ! 1; 7— »- — — - j j\ 9 -, ';•} : \ •i / , i 7_^ _. lAi ^- - 1 A ^1 — ¥t " , " "l > i t-i . ( y N m kWf sm < / MM ITB fO i« m UTK s :t — / ' 1 : ". ,-..-t > / ,,_ 1 ^-* J / .; /■ . .■ rfr r i ^ 1 .^ ? _^ t ( 1 i. f (f 3 / 2 "i:f / 1A fl, 'e I 1/ < 7/ * 7/5 i ( ■h // /^ ^< qL / /; ^/ ?,T / ? ^A 10. 9 ?^ ^r! rn ?7 f- ^ f YC 7> to r/^ //< ",•> o, c r7 ^ sc ■(7/i '^_ ^ ^ i2 4 / C ?/ :li A'l ^^, ^m fG <7h /f^ '(? ^ V?' /^ 2i ?; r. n. \ Ir, f S tJ ^n :: ' ■? T ' T „_ — "" 4-, '»!' ^ :\ ^ " • ■ ■■--.- ' ■;_-/_ - -■ ----• -p- F^ i-^ -.1. l^'i ' i 1 1- r fe ^ — .t k - 1 ^-vi f- ' I ' JL P 1... _ ( >- * -? v~ tsXT ^ ft. 1 — ,^. }•;■ > -^ ) "^ 5^ b K •^ i ■ % 1 r ' — "*~r j;;j ^ i r S ^ 1 ^ 'i') i|i| I'i: i M ,i •^ — :i ■ -j ^ h J • !■'! E^' ^ - *^ ^a "^ \ — _ ,r^ l-'-i. K ^ -; i ■ ' ^ ■^ %\ — ' i: ' 15] u^ ■ « 5 , -!] K _ /f •r-T L.I ^S ^ & r ' ' \ vT ""' , i"" ^ i^; :;:' "\ ^*>N , .7- I'-t J_i' T % - ■ ^ \ ^ r -i "> <0 ( ^rt \ '_ W ^ — l:-' ,] :^' ■ ai ""''■• " ; L- ' t\-. c:: N T '■ 4 -:|- 1 ~ — -- s > : i; t - : t '- , ' '■" / T ;, ; I 1 :— i-:- ..(^ f' t 7 >w f- ^1 \ ■7- - K ^ k: -J 1 r /- U •~-, xl' 'a 1 i' ^ 4^ -* -^ %^ i. ^_; _ ttH i;'i ^ _ ,1. T 4 i / >-. ^ »<^ J.i / ' ■ : - /, / A „. ^\ 7 .^ „ '^ 0. M-f - / / '■\^ i < >' r^ > t: ; M- / W / <^ J. Vj — ^ i,^ rT ii/^ t!' l"i. ■ f I 1 •: y f ■/ / \ J i u. ) n''> A ■ I ' \ I -I £ /^ T'> k rf < > ^- ^ t ■ ^ y !^ 7 ' / / f jl T / rl ^ ; ; fi" / •^ ■ ' r V s 4 '^ V / / R- V ■ ''i \ 1 i 7 f-. / / A ^ , / / S : ^-j: • ^ ■vj ') I \ '■ '/ 1 / i y n i ;/ 1 f. ' 'ii +1 .'■ :"4; ri'l i"*' "c^ ^ V (^ 'p- \ t / / i' ■-* 7 / ^ 1 : 1 '"-1 ^ c; N N \ -V 1 .-r- P 4 y / '} ) =. i^f p ^v; , ^ 1 ,1 -H N ^ / / .-' \ ■ ■ i li / / ii: A .A - .^ A — 7 f _ 'N ^ / " 1 / V /^ / Q r r7 ?if> I tt ^ \ S / y < >' 1* 1 — . —

— « _■• '^^^ ?■ ■; ■'■ • . >0 I c V ^ ? -^ \ s ) — " ,< y^ ■f /' A — — — « — ,^^ 1^ v/ "4 J • ^■-1 -^ r _)'0 >,- __ . -- y -<(; ) V — -. _ <^ p Trt -§ t -t }- ' 7 -- — rin: -_j_ z ?1' N -*J ;:■- , ■: / L • ;,i ^ l'^ (< > \ - 1 / '^r --*:!■ L ' i c y — H mo ML. AW ISOR 1 •Irl f- / a IM» nE (« tONJ lUIK S l;:^ / r ; ^ J , , L_ -7 L _1 __ ^-^ — — — -:_ _ . — — . _— -_. _ — _ — , — — — — — "7 A- — , — — ' — ' — — — — — ' — — — _J -■ - — — ' — — 'iz- ( < - '.- f-' ; 1 r -} ^ -I . Y ) - ^ /, 7 15 / i/> 7'' o o f n V ir. c ^.i a ^'^ ti' vf, V a; R( ?^i '■^ ?(0 /^ ffi\ r, ( Of : 'o r- ■s\ ir ^ Tf^ t //^ A ')a rr. 1 fl 'n\ P ^ vAa 1 -: ^i ft W f ?'r?/ \n 2'> 'Oi 2d / ■2Ji c r 2C fr C^ 2- n/ 7k P /h: ib' ?/ ^-"' ni /7 O / "1^ a 4 '>} — r<\ _ V). "if )^ r/r ri l^' -^ ) r 1 _ m ■^rt '- . r- _r -;- i--4i ^ -t;^ •-3H- ^T-i -^■^ -n-* ■^r ?" -^"; j^ - - - •7 j-_ , r r^ r rk ^ . *-■ .L.- " ! o . _^ fn -^ Q. >- I-— -~f n ■A ) . i ■V « V > '-->-<. ^ .^^ ■) : C -^ ^ -J- c r u ' \ ~s ;-f A — — ._ — - ■'^ r L — c^ ■* -- y hr* ^Z" a , ^ ■y / ^ >"' ■ tl ^ iS V — — — _ >S 1 : .; -V \ A -',- )L a / y y * <. ^ § - i(5 t^ X ^"n»5 vS \. NA IW w WI^ (IRY ' - 1 k1 n fe< / ^ %. ./ - * --_ ■C i':.* t:i. — — y— — — t-^ — — r — . : ; ; — -— — - ^_ — _ — - — -— — — _ i t~- — — — — — " -J - -r •— — — - ^ ■- — — ■ — — ' — : - -7- - — ' — — — — — , - : ■t n rt' -k It - ' .Li /^ ^ ^ - ( J^V V / N, - ">' ::; ' / /" < / s \ Oi J •■ ! ■3 ( . / [ / V -i S \ -/ f 1 ,J Ki — ::■ , / / f f \ ; I ) / . i / s 1 J ^ ^ ^ — - ; J L r" I ^ C ' -<^ 7' ( P^ f 1 > r / h \ --ij 'T 5 \% .n. V A \ / / / / nip^ "V, -/^ 9 'r- V* -i Jf - /J -Is J K L / v.. Ui- i '/ * ■; 1^ r^ 5^ i / / - 3t \^ ~ i^ s< ^■rk- / 1i / c •<. ri' ^u - 16 >•• ^t 1^ 1 K i / Y r "^ r i- "• 1 , >- 0'- ■>s \A Lj / T/^ ^ -fi ^ : Js^ > ' / '•> 1 r ^T ' — — " S 'i: / -{ r < { / ^ ^ n \ r\ / ^ / / A ^ — u U ( y ^ f /■ / L / < > / A 7 rr: 'r / / / L ^--: ^ o / / / .t / i \ /' ""•_ ' : - /^ r / ^ ^ f ^ 5 i : : ■. ;" ff i •- *-* . ■4 8 — i ( ) ^ i > ? / ? ^-1 ; ' A Yx )/f\ n f m Yr. r} r. c < C 7i? r? -- — 1 1 ■-■ - - '^'- ^'- ■ ft Q/ (n x> ^ - I 'f1 ef t o, f lit T ^/ :. <: y/, 7^ >(0f 3 /A ( If ( iL ? m 3J -.'ij r" /. J.O 0/ 7 K ^1£ . : 7/ )e, r?f "Vi y ■Y5 n )tr c hhr ■l^ytf n,v Vl^,"! n Ik 7 J 7> •y; ^/ r ■3: (0? r th fO h ^n J ?/ ?-, 6\ ^ = n: '€L 111 ohk ' ri ^ 2fe V )Jnt , t. f 5 V ■^ V — — ._ H ) vi ^"S » -'■ 0- --v ■^ ■i- 1 "X X {7 — _- _ V Vl --? 5- -0 hi >*i-^ ^ . r 1 > \ j)mr «n Rffi Y - ?5 He n -( i^ .^ ^ N. ^ 1 \ C )m int RAf RON |\uni s ■-:! ^(J; • 'f 1 5- ~~- :r' ci )>v< >-. ■K. \, 1 s^ ^ ' 7^ ^ k < ^ \ s ^ iiii t p ^ 5. Sv A \ ^1 < ^ . / N V > 73 ./ -; ' X ^ K ^1 1 r .:.r !.■ a. ..^ 1 V -r )" o y' A ^ > ;4 ( < / / ^ -N « /i ■ "-■-T ^ ~ i / i f^ sg a f-^ ^i .1- 2^ ^ / r 1 / T •--. ^ 3i ) ■ n -i ■J \ \ / / / - ^i? -< & h' s\ ^ -., . > r 1 7^ "/J ^ •-- _, ^,' r --i ( r ■ > r \ ( ?. , /.I L :i i 7^ > i^ -^ ^ ^ A • •i f- s K, _ / # 5^ „ (^ 7 -Tt __ [^ — .c — i^ 4 — — -^ r. \ r^ /- ^1. K'^ ^ m ?-- % -■ i — — — t — ^ ~ ^ __ d ( ^ P^ ., .r ^ ^^ 9 i^^ A / - ^ — -^ li 1_ ' ■^ — 'v / r^ -i i> ^-f - ry-< >/^ >- '/^ f^ ^ -1 •/ ^ c- ■^ H[ > r ^ -^F hL )C ■^ 'A / '.-t ' 'a; -R; / ) T i ' ^,- ' ' "tt ■ c: » / f / > ' /^ / / :r ■■* ^~■-" t. ■ -tt-t ^ r\ '' 7 / - f"""^ ^ / / > ^,7 / / ;;! — — _■__ / / \ /' \/ ^\} / -' :-.3 p / / :it •- / / i \/ f f _-._ ^ *l / ■ / ; r -■it ( ) / /■ V-tfl ,/ / / V \ f' / ■^ 1 / li / , — ! ■ ill •"^< ^ «. 4 ( ) i f \ / ? . -4 — — — A. nc y^ 7 a f Hi Yr. f^/* %r i <, r. '^( 7 zst "■J 1 -i " i "*t ! a 7>- /r, o j 4 - f f Of N,i 1/ VJ T, 7' //: /> Tf < 2^ 7 /'n d ? Ti n 1 t ^ n^ ¥ in rr, tC] rnr. ^ti r?' (1} 1 z^- iO ?/f !> "- C _.. A-- 1p, i I 'h\ ? ^ rx > Gi ^if (TO )//(9- Y^ » '7 f/r ife _-^ ^ ^ [ an r ¥- =%■ r (f. '-^r. = n. -r) t> ' ^ __ _ .:.:-; - " L^;^ ^ f — — - *v \ y. -' i I i__ "2:^ K "-r V <^ f(J 1 } \ >■- ^ n ^ ^ ) ./ 1 ■< >- '/ s ^ lN _^ — — t Hj < >- ^ c ]-^ -~^ ^ 3:; 'V 1 > "\ = - _ i^ - — r \ y- ■~- -^ V \ \ ''.f M '" ' K :i u J-v s. s \ ?<' ) ■,-,- ./ « •^ [ ] \ ---t ■^ (^ i ^ )'^ s. V /J ■ .-■^ — — 's \ ^^ A ) (. )' -• .c rf^ ■ — ' ( < .L J -1 T — f f r- n V / <- •- "^ c h- / r >^ > ..; 9 -V 1 A > [n / r 1 / ^ .-^ _ 4.'- •\ V 14 / / k ^ _ . \ s i s **^ ( ) / / I ^ ; 1 • 1 V: 4 r)- \ ""■■ /^ '- ';■; } v^ -^ 7/« ^ _ ^ "^ t* } s \ ^ 1 ^ / / *v i «»f ' / •- s f /-^ " \ '1 y / ? / // / ^ X ^ N *< f / 7< ^- -i^ \ 1 *- '-4^ ^^ ^ T > ( . [( V (^ \ . •5: ;^- r« r ^ • V , A 5^ ( I -k ^ ^ / v:: ^ / / ^ / ^ ?- — -^ *"- / f < < / \ T ' - — — — 1 K ) ^ (< ^ • / / /' / f - — — — h[ ], -/ ^ <-: — < t-^ "V, - Ci )■■ ( y "■I 3' / / - - -< >. 1 9 ^ / - r / \ 1 - — - ^ k ^ <« T "■ / / / \/ . — -- — M '^ <; / / / / m.tA ■ 7 < > / } r ft m NAU*C' ISO* » / r ■ / / c )MM rm ; Ft fiAf SON ^un '& -■]■- ( < - / / 1 1 4 / \ / -f r T y A { ■|" / ,^ i . i t ( 7 ^ t f ? /, ? : ^A k?. (« c f c // a: k. ^ t cL ■w ~ — El b i9 V 1 - L ( m rft A til - Qt at Mr/ /r fr-i • 2 12 72 2C 1 - T ^ V'' Y), 2- — \ir,'° wr, /? ?<^ • ^ ft ■9 f ^ro/i 7/ ?/ .t. J ^ — f^ '4 r (- -^ ^ — — r ) -K c >■ \ s — •r . . V 'T - 1 ' ' J- *==! J ^ Sj ■7 \< V (J^ u_ _i. C / 1 -/ i- -L ■^ A — . — ^^ <.f ■♦>. \ ./ I > ^ ^ C y^ ^ -_ — — — — ^ V ^ - - _ — 7^^ ^ ^ 1 ■ ' l.\ -^ - Q WW iti m m f s ^ r\ t^ fO RU low ilTX s u ( Vi P ■^ r *J , ^ hi , .1 .1 ' ■ ■ ■ " * '■ — -^ — " _ - n ^ "J JS r?^ . r) > ■ -u / i'' /■ ^! > ■ / :; L-^ / \ V r ^ /■^ / :; f' / t ] t ^ .■^ r .11 ^^ p»-1 /^ —J &.V i,1 / / £ - ^ r ?■ • --^ -1 ZyC ■4 Mh' . V r ' ^ 6( )°- _! Ev *^ < 5 / / r \ ' , t ,4 ■ ■ • '- 7^ i^ ^ k. ^ ^ y .L C. # ■^ 4'- ti i t-- ^ /. r / N . <^ 7 • < \ ^ / r-* /h -i k-< '-i r vl 5 ^ . 1 [ ] / ./j ^ 1 \ 7 f' ' — i 1 r^ ,-( :> ■ k ^ -^ — ■/ u >- :^ ^■ "X f ' ; 1 •/ ^ .6, <«( ■)! /" 4 t- i. r-l ar' y^ =^ 7^ / if 1 V ^ 0" / f- / ^ / / / ^ ' / / f ? / / J r / s n " / / c ■■ ' ^ J ^ ° < y 1 f { / ) f N / / L r / / / -> f f f / 7 C /: < > t ; ^ / / / < , / ( ) / / / 1 ' ' • A / / t r^ 4 1 / 1 / V < ^ '/ — ( 1 ^ =! _ 4 { ) i f ? / p 1 Af Kli\ ^ (^ y f It. H -.h r, c <• ip y F/ li fn 5. - i n < 2/ a -L -A (A ot si It y- .f< /a; f?' -P '^ ?^ 1,"? > ' / ^ . If- a. n/r J- 7 rv 7 V L p/ a ^ i — — — ~- -•- Q /? '' "i / - UNIVERSITV OF FLORIDA 262 08103 300 2