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6.1 - Uniform flow FIGURE 3.34 over the body W17 L/rce...

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Unformatted text preview: Uniform flow FIGURE 3.34 over the body. W17 L/rce 47¢ ' -J~*A——m—.M‘ , txmuvnunum. - . “.mkmhw. . P44"; / /’7€ fZM/J Source sheet on surface of body, with Ms) calculated to make the body surface a streamline Flow over the body of given shape “ _\Ii£hdMnW-I—Mix-M—'shhuyarmhw34 awn—gum.“ m -.‘._ ,Efiidfik. , --. VVF7<¢IJ V'?‘ I71/(‘jjfl {fir "“Ia')‘d /("jk4' ”46¢” PL, JA/{f‘cc C i , , gr 4 Fflm‘j” Vy/fl"? 7(1) : __, FIGURE 4.10 , ._ __ ._’_ 5’ Van arbitrary shape Simulation of an arbitrary airfoil I v a); h and thickness by distributing a vortex sheet over the airfoil surfacc. ' —\ I zVé/aCz// Pu}1fi{;/ i 773-5 Viv-(fig. S‘t’rtgfl - 1 y ,e‘m'? C , . I) :9 /r(‘., [27437-1 lb, 7‘7C 7544., ”be 71p Vé’r7('¢ (J X “9' ”A” 7£Vr /"‘/74 A; (pr kph-Kffi‘fij) ééw/VU "’2’ (7’274- /) ’ F/I’jy (H 4fl/7/47X'-M<7[C 7‘76 Xi’an-(74'). ‘I’J { Jr/I'VJ _ y‘JL n f/(f W‘fiI/J',‘ W __ —/7if6 yin—’44“ (jf(s7’r/ I4) 7 “war; 4 F‘eg/ h 1.5;, </ /F‘-/"("/ ¢/ . r4 J), flvo-va/ J ’5 —— _._/__ 0% 2;.[ag XJK/KJ‘: J ‘ ‘ x-‘y' . - ) MM %~7L«I(H (vaerc ' 5’.“(¢ fl/ VJ 7L76 fltq-K/J 1875/9-(6(C flinhf ’5' {m271 ya”! ”(.17/ J) l—V..c 5c7‘ *(z er/xwrz Pfi/zfijg‘r/ /H///Ac(/ {7‘ A M025») : Jéég : _;§ £f5’3) M" (/4) M f rflJ—Wwfiz/ {(-59 25 I Ifiej7/C’fi7/ 5"? (<4! _f/7€h(/ J’ (fifl Vf/I’é‘ 72/. /4/27‘-n,}{;5 J / a1 ’1 ‘94.! "I Ma f; +(c / Vf/fé'I/Jr ”firm—H. 5:... 1(4Hv fi<vfi («If “new?" 4.2;“; .‘ “Mfg : £5 :: h 7—4175 1,ng (1": (0) "7L (// [:7‘774’12/ ”injyi WC 5947/), (Affi/(ag (fl—n a) fix (m-/) 915' 7"?"5 {Va-374’ V/flPJW7IJ“ F 12,—- 7/76: 74"”7/ (fH‘X'P'; ‘V'C (“fl/ac /);£:fl (E) *_'————_.._ pin/g A”; 1/7 94:74:01, 49.14 17 Afiflpwh l/yr7l7k 5%4 f7} 9/- — .11 145’ HGURE 4.9 Tangential velocity jump across a vortex sheet. Vt /’61 it), /',-,5~ {/g VI ryly X J 4 z t 7” ...
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