10_21_09 - . W (Jae. 6 MW. #6 Jae. :olmlm 262:5 (2 m. WHCOX...

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Unformatted text preview: . W (Jae. 6 MW. #6 Jae. :olmlm 262:5 (2 m. WHCOX up ’Harwug}? [2.7 area/uglmfi IZA- -=- Do problemg, 12¢, 12312.10, 12.12, 12.5, :24}, Iz-ancl 12%. 0 lOlHloq '- EJ’G—Q‘Llaj C3 llfiaef‘ e> 10121109 ' More. Po‘J’fl-O'élai giaw Paw?!” a, gfilmoger- PM!» rfia-éxo/p .I if. 50 SHEETS 22-142 100 SHEETS 22-!“ 200 SHEETS 22-141 6 m “an; 2'— ‘ [Umbme + U‘aQ- Y'EI-va m I331 way I g “m + {1:} §oarfim we. Wzéwm UQCQ'Q‘BE F‘ 3 [Zil- fZ. = 2.17; L; ‘- I] r" to" r 1502;," r f r" m: 'i .‘ “’3” W Va: $r-"!/¢.'*}f a LE..ng 1(7):; L 6% Izoéz‘z hum-=3 ‘3) {-329 v) imh (U, film-5%? figxwflfifidg Ur/E,e\$c) UEME'Q) g _ZU‘D‘6’”‘*§+§%§ “’5 (3 13> 5mg:- ETTQAm .. i" ,1 ‘9‘: 5‘“ {WE (FE4T?Uw} ‘P 2‘ 6+;3n3l30q ‘Pfli'flfiifi 0"" CA} “kiw- i; d. a“ |”"L’-?C& For F“: 47TEUM, 63's]? 1) =3? 9:463" (élnfiki. Pagan FEW larger VERIQGIC’ '1 {HA5 {3&75‘33'13g7‘m F’C’Mii’ flaw"; .,'4§.)¢ihi¢ wHa-i r1: “J Cant-<3 "g 54%";“Mwag €.£p‘~::MEEs-¥”l2)fl. Figure 11.13: Dividing streamlines for rotating-cylinder flow; [‘0 = 41rRU is the critical circulation; 0 denotes a stagnation point. 50 SHEEF5 22-362 300 SHEEI‘S 22-344 200 SHEE'E'S 2244? @ Force Co Mpui-N‘ééaq w Eo=Lea4rmaj Jlrxjcf 5pm»; "afiavmi." Uw '- ioulfjf‘ Vagaéd‘i‘f -- Pramdrfl. \ éplflb Hwy-Mam Um - higher VEJQQ-JY m Edwer” f; (“g-42%.: MC. 3,“. I'I‘gfiukghfié; L; \Nfi; W42 LA 11:} 2:33: Mai- 26ft} cit-.33 {ha €323 45L w-zn-su-."-”?-¥a"< - itch] abjL—rl: "Mic; Vw-flxm bx4~“-jv‘:t}:-J ma wmujé cw 93'1"!” :3 irvfiJ' —2£ar'cie, )0 cf- =— \f'. If: ' L D —-————, C — 11.136 %pU2(2Rb) " §pU2(2Rb) ( ) CLE Jhere b is cylinder height. The quantities L = Lb and D = Db are total lift and drag, espectively. In the experiments, the cylinder rotates in the clockwise direction with angular elocity 1», so that the circulation is 1‘ = —21rwR2 (11.137) 1‘ into page L out of page Figure 11.15: Various motions of a baseball. ...
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10_21_09 - . W (Jae. 6 MW. #6 Jae. :olmlm 262:5 (2 m. WHCOX...

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