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- きよはる あみおか
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1 11 11
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3 A A A A ii -
4 % 30% 40% 1-2 RCu R Cu =tan -1 Cu/Cm - 1 -
5 Cm s Cp2-5 s=(r5-r2)/cos 2=0.8 R2/cos 2 Cp2-5=1-(R2/R5) 2 =0.69 R 2 R s=(r3-r2)/cos 2 - R3cos 3v+(R5 2 -R3 2 sin 2 3v) 0.5 =0.1R2/cos R2[ -cos 3v+(2.68- sin 2 3v) 0.5 ] Cp2-5= 1-(R2/R3) cos 2 3v /[(R5/R3) 2 - sin 2 3v] (R2/R3) 2 = [1- cos 2 3v /(2.68- sin 2 3v)] R 3 3v
6 R R CFD CFD - 3 -
7 CFD (b) Total-Static Total-Total Total-Static t Total-Total 1-3(a) 1-3(b) A t A - 4 -
8 C m W 1-6 A A THR 1-5 HIGH FLOW LOW FLOW 1-7(a) 1-7(b) t 1-7(c) i d - 5 -
9 1-8 p p p t 1-8(b) t - 6 -
10 Yoshinka
11 0.40 Hunziker Gyarmathy Klassen Wood Cumpsty Kmecl Dalbert 20 3 CFD - 8 -
12 Senoo Osborn Sorokos Senoo 8 10 Hayami Umemoto Aminei Engeda 1-9 Krain 5 Wake Wake 1-10(a) 1-10 (b) 1-10(c) - 9 -
13 Senoo Ishida Mounts Brasz Dawes Dalbert CFD CFD
14 CFD W 4/W2 (pn-p )/(P 0 -p ), =2 2m,n=3 6 L
15 u Nd 0 / 1 (2 2 /60 : (rpm)) X 2m =1.1 2 h T 01*((P 02/P01) ( -1)/ )-1)/(T 06-T01) 2m R =1.10R 2 T 01*((P 02m/P01) ( -1)/ )-1)/(T 06-T01) 6 C pt0*((p02/p01) ( -1)/ )-1)
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