27 1: Lewis $Le_{i}$ $\mathrm{c}\mathrm{h}_{4}$ CO $\mathrm{c}\mathrm{o}_{2}$ $\mathrm{h}_{2}$ $\mathrm{h}_{2}\mathrm{o}$ $\mathrm{n}_{2}$ O2 $Le_{i}$
|
|
- ほのか えいさか
- 7 years ago
- Views:
Transcription
1 (Naoto YOKOYAMA)1 (Kana SAITO) (Jiro MIZUSHIMA) 1 (Peters 1984) (Kida and Goto 2002) (Donbar et al 2001) ( 2002) Navier-Stokes (Nada et al 2004) Everest et al (1995) Rayleigh - 2 (1998) Skeletal (2004) / - $k-\epsilon$ Large Eddy Simulation 6 4 l nyokoyam@maildoshishaacjp
2 27 1: Lewis $Le_{i}$ $\mathrm{c}\mathrm{h}_{4}$ CO $\mathrm{c}\mathrm{o}_{2}$ $\mathrm{h}_{2}$ $\mathrm{h}_{2}\mathrm{o}$ $\mathrm{n}_{2}$ O2 $Le_{i}$ Dufour ( ) Soret ( ) $\rho$ $u$ $T$ $Y_{i}$ $\frac{\partial\rho}{\partial t}+\nabla\cdot(\rho u)=0$ (1a) $\frac{\partial(\rho u)}{\partial t}+\nabla\cdot(\rho uu)=-\nabla p+\nabla\cdot\tau$ (1b) $\frac{\partial(\rho T)}{\partial t}+\nabla\cdot(\rho ut)-\nabla\cdot(\lambda\nabla T)=-\sum_{i}1\underline{1}h_{i}\omega_{i}\overline{\overline{c_{p}}}\overline{c_{\mathrm{p}}}$ (1c) $\frac{\partial(\rho Y_{i})}{\partial t}+\nabla\cdot(\rho uy_{i})-\nabla\cdot(\rho D_{i}\nabla Y_{i})=\omega_{i}$ $(1\mathrm{d})$ $p$ $R$ $W_{i}$ $p=$ $\tau$ $\rho RT\sum_{i}Y_{i}/W_{i}$ $I$ $\tau=\mu(\nabla u+$ $(\nabla u)^{t}-2/3(\nabla\cdot u)i)$ $= \sum_{i}y_{i}c_{\mathrm{p}i}$ $h_{i}$ $h_{i}=h_{i}^{0}+ \int_{t^{0}}^{t}c_{pi}(t)dt$ $\omega_{i}$ CHEMKIN(Kee et al 1996) $\lambda$ $D_{i}$ $\mu$ (Smooke et al 1991) $=A(T/T_{0})^{07}$ $\rho D_{i}=Le_{i}^{-1}(\lambda/\overline{\%})$ $\mu=pr(\lambda/\overline{c_{p}})$ V $A=258\cross 10^{-5}\mathrm{k}\mathrm{g}/(\mathrm{m}\cdot\sec)$ Prandtl $Pr=075$ Lewis 1 $Le_{i}$ 6 4 (Jones and Lindstedt 1988) $\mathrm{c}\mathrm{h}_{4}+\frac{1}{2}\mathrm{o}_{2}arrow \mathrm{c}\mathrm{o}+2\mathrm{h}_{2}$ $\mathrm{c}\mathrm{h}_{4}+\mathrm{h}_{2}\mathrm{o}arrow \mathrm{c}\mathrm{o}+3\mathrm{h}_{2}$ (2a) (2b) $\mathrm{h}_{2}+\frac{1}{2}\mathrm{o}_{2}=\mathrm{h}_{2}\mathrm{o}$ (2c) $\mathrm{c}\mathrm{o}+\mathrm{h}_{2}\mathrm{o}=\mathrm{c}\mathrm{o}_{2}+\mathrm{h}_{2}$ $(2\mathrm{d})$
3 $v_{\mathrm{c}\mathrm{h}_{4}}$ $\mathrm{m}$ $\mathrm{k}\mathrm{g}$ $\mathrm{s}\mathrm{e}\mathrm{c}$ $\ovalbox{\tt\small REJECT}$ $\mathrm{m}\mathrm{o}1$ 28 2: $A_{i}$ (a) $44\cross 10^{11}$ $126\cross 10^{5}$ $(\mathrm{b})$ $3\cross 10^{8}$ $126\cross 10^{5}$ $(\mathrm{c})$ $25\cross 10^{16}$ $167\cross 10^{5}$ $(\mathrm{d})$ $275\cross 10^{9}$ $838\cross 10^{4}$ 1: $\Omega_{j}$ Arrhenius $\Omega_{\mathrm{a}}=A_{\mathrm{a}}[\mathrm{C}\mathrm{H}_{4}]^{1/2}[\mathrm{O}_{2}]^{5/4}\exp(-E_{\mathrm{a}}/RT)$ $\Omega_{\mathrm{b}}=A_{\mathrm{b}}[\mathrm{C}\mathrm{H}_{4}]$ [H20] (3a) $\exp(-e_{\mathrm{b}}/rt)$ (3b) $\Omega_{\mathrm{c}}=A_{\mathrm{c}}[\mathrm{H}_{2}]^{1/2}[\mathrm{O}_{2}]^{9/4}[\mathrm{H}_{2}\mathrm{O}]^{-1}T^{-1}\exp(-E_{\mathrm{c}}/RT)$ (3c) $\Omega_{\mathrm{d}}=A_{\mathrm{d}}[\mathrm{C}\mathrm{O}][\mathrm{H}_{2}\mathrm{O}]\exp(-E_{\mathrm{d}}/RT)$ $(3\mathrm{d})$ $[\cdot]$ $A_{i}$ $E_{i}$ l 2 $\nu_{ij}$ (2) $j$ (1) $\omega_{i}=\sum_{j}\nu_{ij}\omega_{j}$ 6 (Lele 1992) Navier- Stokes (Baum et al 1994) 1 $d=2\cross 10^{-3}\mathrm{m}$ $Y_{\mathrm{C}\mathrm{H}_{4}0}=1$ $T_{1\mathrm{o}\mathrm{w}}=300\mathrm{K}$ $T_{1\mathrm{o}\mathrm{w}}$ $v\mathrm{c}\mathrm{h}_{4}=40\mathrm{m}/\sec$ $Y_{\mathrm{O}_{2}0}=0232$ $Y_{\mathrm{N}_{2}0}=0768$ $v_{\mathrm{a}\mathrm{i}\mathrm{r}}=4\mathrm{m}/\sec$ $T_{\mathrm{h}\mathrm{i}\mathrm{g}\mathrm{h}}=2000\mathrm{K}$ $t<50\cross 10^{-4}\sec$ $T_{\mathrm{h}\mathrm{i}\mathrm{g}\mathrm{h}\mathrm{i}\mathrm{n}\mathrm{i}\mathrm{t}}=2250\mathrm{K}$ $T_{\mathrm{h}\mathrm{i}\mathrm{g}\mathrm{h}}$ 1 $Re\sim 8\cross 10^{3}$ Reynolds Damk\"ohler $Da\sim 4\cross 10^{7}$ 4 Runge-Kutta
4 t=48 $\cross$ 10-3sec& \acute 2 $t=48\cross 10^{-3}\sec$ $0\leq r\leq 12\cross 10^{-2}0\leq z\leq 95\cross 10^{-2}$ $5\cross 10^{-3}\leq z_{\sim}<225\cross 10^{-2}$ $J$ $z\sim 8\cross 10^{-3}\mathrm{m}$ $\cross$ $\leq z_{\sim}<4\cross 10^{-3}$ 2 ( $2(c)-(g)$ ) - l $\backslash ^{\backslash }$ ( $2(a)(b)$ ) 32 Bilger(1988) $Z= \frac{2y_{\mathrm{c}\mathrm{h}_{4}}/w_{\mathrm{c}\mathrm{h}_{4}}+(y_{\mathrm{o}_{2}0}-y_{\mathrm{o}_{2}})/w_{\mathrm{o}_{2}}+(y_{\mathrm{c}\mathrm{o}}/w_{\mathrm{c}\mathrm{o}}+y_{\mathrm{h}_{2}}/w_{\mathrm{h}_{2}})/2}{2y_{\mathrm{c}\mathrm{h}_{4}0}/w_{\mathrm{c}\mathrm{h}_{4}}+y_{\mathrm{o}_{2}0}/w_{\mathrm{o}_{2}}}$ (4) $Z= \frac{y_{\mathrm{o}_{2}0}/w_{\mathrm{o}_{2}}}{2y_{\mathrm{c}\mathrm{h}_{4}0}/w_{\mathrm{c}\mathrm{h}_{4}}+y_{\mathrm{o}_{2}0}/w_{o_{2}}}=z_{\mathrm{s}\mathrm{t}}$ (5) b $D_{i}$ $D$ 3 $Z_{\mathrm{s}\mathrm{t}}$ $\rho\frac{\partial Z}{\partial t}+\rho u\cdot\nabla Z=\nabla\cdot(\rho D\nabla Z)$ (6) $Z=Z_{\mathrm{s}\mathrm{t}}$ (6) $\rho\frac{\partial Y_{i}}{\partial t}=\frac{\rho}{le_{i}}\frac{\chi}{2}\frac{\partial^{2}y_{i}}{\partial Z^{2}}+\omega_{i}$ (7) $\chi$ $\chi=2d \nabla Z ^{2}$ $D_{i}$ 2 (6)
5 30 2; $(t=48\cross 10^{-3})(a)$ (b) (c) (d) ) (e) (f) (g) H $z$
6 31 3: 48 ) $\cross 10^{-3}$ $Z_{\mathrm{s}\mathrm{t}}$ $- \sum_{i}h_{i}\omega_{i}$ ) $(t=$ ( Lewis 1 Burke-Schumann $Z\leq Z_{\mathrm{s}\mathrm{t}}$ 0 $Y_{\mathrm{F}^{\backslash }}=\{$ $Y_{\mathrm{F}0}(Z-Z_{\mathrm{s}\mathrm{t}})/(1-Z_{\mathrm{s}\mathrm{t}})$ $Z>Z_{\mathrm{s}\mathrm{t}}$ $Y_{\mathrm{O}_{2}0}(1-Z/Z_{\mathrm{s}\mathrm{t}})$ $Z\leq Z_{\mathrm{s}\mathrm{t}}$ $Y_{\mathrm{O}_{2}}=\{$ 0 $Z>Z_{\mathrm{s}\mathrm{t}}$ $Z$ $Z\leq Z_{\mathrm{s}\mathrm{t}}$ $T-T_{1\mathrm{o}\mathrm{w}}\propto\{$ $1-Z$ $Z>Z_{\mathrm{s}\mathrm{t}}$ $t=48\cross 10^{-3}$ 4 Burke-Schumann Burke-Schumann l $=Z_{\mathrm{s}\mathrm{t}}$ 4 Z G 0 3
7 $\dot{\mathrm{b}}_{\tilde{\mathrm{t}}}$ $z$ $T_{:}$ $Y_{\mathrm{C}\mathrm{H}_{4}}$ $Y_{\mathrm{O}_{2}}$ 4: $Z$ Burke-Schumann $Z=Z_{\mathrm{s}\mathrm{t}}$ $(t=48\cross 10^{-3})$ $Y_{i}$ (7) $Z$ $\chi_{\mathrm{s}\mathrm{t}}$ } $=Z_{\mathrm{s}\mathrm{t}}$ 5 Z $\xi$ (a) (b) $\xi=0$ $r$ $n$ $\varphi$ $\varphi=\nabla\cdot u-n\cdot\nabla u\cdot n$ $5(a)$ $\xi\leq 8\cross 10^{-3}$ 2 3 $z_{\sim}<7\cross 10^{-3}$ $5(b)$ \mbox{\boldmath $\xi$}\sim $<8\cross 10^{-3}$ $5(a)10^{-2}<\xi\sim<\sim 25\cross 10^{-2}$ $5(b)$ 2 3 $10-2\sim\sim<z<225\cross 10^{-2}$ $5(a)$ 3 $6(a)$
8 $\mathfrak{c}\backslash$ 33 $Z=Z_{\mathrm{s}\mathrm{t}}$ 5: (a) (b) $(\mathrm{x}10^{3})$ (b) ( ) 6: (a) 2 up ( )down b ( )
9 34 $(r z)=(28\cross 10^{-3}2088\cross 10^{-2})(\xi\sim 1499\cross 10^{-2})$ $\eta$ $\eta=0$ 3 2 $6(b)$ 2 $\chi_{\mathrm{s}\mathrm{t}}=2d \nabla Z _{\mathrm{s}\mathrm{t}}^{2}$ $(r z)=(302\cross 10^{-3}1388\cross 10^{-2})(\xi\sim 2201\cross 10^{-2})$ $\grave{\mathrm{j}}\ovalbox{\tt\small REJECT}$ Burke-Schumann $\langle$ Lagrangian (Pitsch 2000) 3 $\Delta$ Baum M Poinsot T and Th\ evenin D (1994) Accurate boundary condition for multicomponent reactive flows J Comput Phys
10 ) ) 35 Bilger R (1988) The structure of turbulent nonpremixed flames In Twenty-Second Symposium (Intemational) on Combustion pp The Combustion Institute Pittsburgh Donbar J M Driscoll J F and Carter C D (2001) Strain rates measured along the wrinkled flame contour within turbulent non-premixed jet flame Cornbust Flame Everest D A Driscoll J F Dahm W J A and Feikema D A (1995) Images of the two-dimensional field and temperature gradients to quantify mixing rates within a non-premixed turbulent jet flame Combust Flame Jones W P and Lindstedt R P (1988) Global reaction schemes for hydrocarbon combustion Combust Flame Kee R J Rupley F M Meeks E and Miller J A (1996) Chemkin-III: Afortran chemical kinetics package for the analysis of gas-phase chemical and plasma kinetics Technical Report SAND Sandia National Laboratories Kida S and Goto S (2002) Line statistics: Stretching rate of passive lines in turbulence Phys Fluids (2004) ( $\mathrm{b}$ Lele S K (1992) Compact finite difference schemes with spectral-like resolution $J$ Comput Phys Nada Y Tanahashi M and Miyauchi T (2004) Effect of turbulence characteristics on local flame structure of $\mathrm{h}_{2}$-air premixed flames J Turbulence 5 16 Peters N (1984) Laminar diffusion models in non-premixed turbulent combustion Prog Energy Combust Sci Pitsch H (2000) Unsteady flamelet modeling of differential diffusion in turbulent jet diffusion flames Combust Flame Smooke M D Wess J Ruelle D Jaffe R L and Ehlers J (Eds) (1991) Reduced $\mathrm{p}\mathrm{p}$ Kinetic Mechanisms and Asymptotic Approirnations for Methane-Air Flames $1-$ $28$ Springer-Verlag (2002) (6 ) Djamrak D (1998) 2 $\mathrm{b}$ (
Effect of Radiation on a Spray Jet Flame Ryoichi KUROSE and Satoru KOMORI Engineering Research Laboratory, Central Research Institute of Electric Powe
Effect of Radiation on a Spray Jet Flame Ryoichi KUROSE and Satoru KOMORI Engineering Research Laboratory, Central Research Institute of Electric Power Industry (CRIEPI), 2-6 - 1 Nagasaka, Yokosuka-shi,
More information$\hat{\grave{\grave{\lambda}}}$ $\grave{\neg}\backslash \backslash ^{}4$ $\approx \mathrm{t}\triangleleft\wedge$ $10^{4}$ $10^{\backslash }$ $4^{\math
$\mathrm{r}\mathrm{m}\mathrm{s}$ 1226 2001 76-85 76 1 (Mamoru Tanahashi) (Shiki Iwase) (Toru Ymagawa) (Toshio Miyauchi) Department of Mechanical and Aerospaoe Engineering Tokyo Institute of Technology
More information(Mamoru Tanahashi) Department of Mechanical and Aerospaoe Engineering Tokyo Institute of Technology ,,., ,, $\sim$,,
1601 2008 69-79 69 (Mamoru Tanahashi) Department of Mechanical and Aerospaoe Engineering Tokyo Institute of Technology 1 100 1950 1960 $\sim$ 1990 1) 2) 3) (DNS) 1 290 DNS DNS 8 8 $(\eta)$ 8 (ud 12 Fig
More information60 1: (a) Navier-Stokes (21) kl) Fourier 2 $\tilde{u}(k_{1})$ $\tilde{u}(k_{4})$ $\tilde{u}(-k_{1}-k_{4})$ 2 (b) (a) 2 $C_{ijk}$ 2 $\tilde{u}(k_{1})$
1051 1998 59-69 59 Reynolds (SUSUMU GOTO) (SHIGEO KIDA) Navier-Stokes $\langle$ Reynolds 2 1 (direct-interaction approximation DIA) Kraichnan [1] (\S 31 ) Navier-Stokes Navier-Stokes [2] 2 Navier-Stokes
More information: u i = (2) x i Smagorinsky τ ij τ [3] ij u i u j u i u j = 2ν SGS S ij, (3) ν SGS = (C s ) 2 S (4) x i a u i ρ p P T u ν τ ij S c ν SGS S csgs
15 C11-4 Numerical analysis of flame propagation in a combustor of an aircraft gas turbine, 4-6-1 E-mail: tominaga@icebeer.iis.u-tokyo.ac.jp, 2-11-16 E-mail: ntani@iis.u-tokyo.ac.jp, 4-6-1 E-mail: itoh@icebeer.iis.u-tokyo.ac.jp,
More information44 $d^{k}$ $\alpha^{k}$ $k,$ $k+1$ k $k+1$ dk $d^{k}=- \frac{1}{h^{k}}\nabla f(x)k$ (2) $H^{k}$ Hesse k $\nabla^{2}f(x^{k})$ $ff^{k+1}=h^{k}+\triangle
Method) 974 1996 43-54 43 Optimization Algorithm by Use of Fuzzy Average and its Application to Flow Control Hiroshi Suito and Hideo Kawarada 1 (Steepest Descent Method) ( $\text{ }$ $\mathrm{m}\mathrm{e}\mathrm{t}\mathrm{h}_{0}\mathrm{d}$
More information多孔質弾性体と流体の連成解析 (非線形現象の数理解析と実験解析)
1748 2011 48-57 48 (Hiroshi Iwasaki) Faculty of Mathematics and Physics Kanazawa University quasi-static Biot 1 : ( ) (coup iniury) (contrecoup injury) 49 [9]. 2 2.1 Navier-Stokes $\rho(\frac{\partial
More information106 (2 ( (1 - ( (1 (2 (1 ( (1(2 (3 ( - 10 (2 - (4 ( 30 (? (5 ( 48 (3 (6 (
1195 2001 105-115 105 Kinki Wasan Seminar Tatsuo Shimano, Yasukuni Shimoura, Saburo Tamura, Fumitada Hayama A 2 (1574 ( 8 7 17 8 (1622 ( 1 $(1648\text{ }$ - 77 ( 1572? (1 ( ( (1 ( (1680 1746 (6 $-$.. $\square
More information(Kazuo Iida) (Youichi Murakami) 1,.,. ( ).,,,.,.,.. ( ) ( ),,.. (Taylor $)$ [1].,.., $\mathrm{a}1[2]$ Fermigier et $56\mathrm{m}
1209 2001 223-232 223 (Kazuo Iida) (Youichi Murakami) 1 ( ) ( ) ( ) (Taylor $)$ [1] $\mathrm{a}1[2]$ Fermigier et $56\mathrm{m}\mathrm{m}$ $02\mathrm{m}\mathrm{m}$ Whitehead and Luther[3] $\mathrm{a}1[2]$
More information42 1 ( ) 7 ( ) $\mathrm{s}17$ $-\supset$ 2 $(1610?\sim 1624)$ 8 (1622) (3 ), 4 (1627?) 5 (1628) ( ) 6 (1629) ( ) 8 (1631) (2 ) $\text{ }$ ( ) $\text{
26 [\copyright 0 $\perp$ $\perp$ 1064 1998 41-62 41 REJECT}$ $=\underline{\not\equiv!}\xi*$ $\iota_{arrow}^{-}\approx 1,$ $\ovalbox{\tt\small ffl $\mathrm{y}
More information20 $P_{S}=v_{0}\tau_{0}/r_{0}$ (3) $v_{0}$ $r_{0}$ $l(r)$ $l(r)=p_{s}r$ $[3 $ $1+P_{s}$ $P_{s}\ll 1$ $P_{s}\gg 1$ ( ) $P_{s}$ ( ) 2 (2) (2) $t=0$ $P(t
1601 2008 19-27 19 (Kentaro Kanatani) (Takeshi Ogasawara) (Sadayoshi Toh) Graduate School of Science, Kyoto University 1 ( ) $2 $ [1, ( ) 2 2 [3, 4] 1 $dt$ $dp$ $dp= \frac{dt}{\tau(r)}=(\frac{r_{0}}{r})^{\beta}\frac{dt}{\tau_{0}}$
More informationチャネル乱流における流体線の伸長
69 d(l/l )/dt y + = 15 Re τ = 18 395 Kolmogorov τ η.1.18 Kolmogorov.65τ η,min 1 Stretching Rate of Material Lines in Turbulent Channel Flow Takahiro TSUKAHARA, Faculty of Science and Technology, Tokyo
More information128 Howarth (3) (4) 2 ( ) 3 Goldstein (5) 2 $(\theta=79\infty^{\mathrm{o}})$ : $cp_{n}=0$ : $\Omega_{m}^{2}=1$ $(_{\theta=80}62^{\mathrm{o}})$
1075 1999 127-142 127 (Shintaro Yamashita) 7 (Takashi Watanabe) $\mathrm{n}\mathrm{a}\mathrm{k}\mathrm{a}\mathrm{m}\mathrm{u}\mathrm{f}\mathrm{a}\rangle$ (Ikuo 1 1 $90^{\mathrm{o}}$ ( 1 ) ( / \rangle (
More information90 2 3) $D_{L} \frac{\partial^{4}w}{\mathrm{a}^{4}}+2d_{lr}\frac{\partial^{4}w}{\ ^{2}\Phi^{2}}+D_{R} \frac{\partial^{4}w}{\phi^{4}}+\phi\frac{\partia
REJECT} \mathrm{b}$ 1209 2001 89-98 89 (Teruaki ONO) 1 $LR$ $LR$ $\mathrm{f}\ovalbox{\tt\small $L$ $L$ $L$ R $LR$ (Sp) (Map) (Acr) $(105\cross 105\cross 2\mathrm{m}\mathrm{m})$ (A1) $1$) ) $2$ 90 2 3)
More information133 1.,,, [1] [2],,,,, $[3],[4]$,,,,,,,,, [5] [6],,,,,, [7], interface,,,, Navier-Stokes, $Petr\dot{o}$v-Galerkin [8], $(,)$ $()$,,
836 1993 132-146 132 Navier-Stokes Numerical Simulations for the Navier-Stokes Equations in Incompressible Viscous Fluid Flows (Nobuyoshi Tosaka) (Kazuhiko Kakuda) SUMMARY A coupling approach of the boundary
More informationTitle 改良型 S 字型風車についての数値シミュレーション ( 複雑流体の数理とシミュレーション ) Author(s) 桑名, 杏奈 ; 佐藤, 祐子 ; 河村, 哲也 Citation 数理解析研究所講究録 (2007), 1539: Issue Date URL
Title 改良型 S 字型風車についての数値シミュレーション ( 複雑流体の数理とシミュレーション ) Author(s) 桑名, 杏奈 ; 佐藤, 祐子 ; 河村, 哲也 Citation 数理解析研究所講究録 (2007), 1539 43-50 Issue Date 2007-02 URL http//hdlhandlenet/2433/59070 Right Type Departmental
More informationTitle 地球シミュレータによる地球環境シミュレーション ( 複雑流体の数理解析と数値解析 ) Author(s) 大西, 楢平 Citation 数理解析研究所講究録 (2011), 1724: Issue Date URL
Title 地球シミュレータによる地球環境シミュレーション ( 複雑流体の数理解析と数値解析 ) Author(s) 大西, 楢平 Citation 数理解析研究所講究録 (2011), 1724: 110-117 Issue Date 2011-01 URL http://hdl.handle.net/2433/170468 Right Type Departmental Bulletin Paper
More informationカルマン渦列の消滅と再生成 (乱流研究 次の10年 : 乱流の動的構造の理解へ向けて)
1771 2011 34-42 34 Annihilation and reincamation of Karan s vortex street (Hiroshi Al anine) (Jiro Mizushima) (Shunsuke Ohashi) (Kakeru Sugita) 1 1 1 2 2 $h$ 100 B\ enard[1] $a$ $a/h>0.366$ Kirm$4n[2]$
More information圧縮性LESを用いたエアリード楽器の発音機構の数値解析 (数値解析と数値計算アルゴリズムの最近の展開)
1719 2010 26-36 26 LES Numerical study on sounding mechanism of air-reed instruments (Kin ya Takahashi) * (Masataka Miyamoto) * (Yasunori Ito) * (Toshiya Takami), (Taizo Kobayashi), (Akira Nishida), (Mutsumi
More informationA Numerical Study on Early Stage of Flame Kernel Development in Spark Ignition Process for Methane/Air Combustible Mixtures Shinji NAKAYA*6, Kazuo HAT
A Numerical Study on Early Stage of Flame Kernel Development in Spark Ignition Process for Methane/Air Combustible Mixtures Shinji NAKAYA*6, Kazuo HATORI, Mitsuhiro TSUE, Michikata KONO, Daisuke SEGAWA
More informationカルマン渦列の発生の物理と数理 (オイラー方程式の数理 : カルマン渦列と非定常渦運動100年)
1776 2012 28-42 28 (Yukio Takemoto) (Syunsuke Ohashi) (Hiroshi Akamine) (Jiro Mizushima) Department of Mechanical Engineering, Doshisha University 1 (Theodore von Ka rma n, l881-1963) 1911 100 [1]. 3 (B\
More information467 468 469 470 471 472 473 474 475 476 477 478 479 480 481 482 483 484 485 486 487 488 489 490 B =(1+R ) B +G τ C C G τ R B C = a R +a W W ρ W =(1+R ) B +(1+R +δ ) (1 ρ) L B L δ B = λ B + μ (W C λ B )
More information液相化学反応を伴う乱流拡散の研究名城大学理工学部研究報告 No.5 21 R 6 R S 1) B 6 2 M =1 Nozzle ID =1.2 OD = x mm 6 mm 6 mm 2 mm M = 1 mm mm 1.5 mm x 1 x = 1 m
1) A Study on Turbulent Diffusion with Chemical Reaction in Liquid Takashi KUBO 1) Abstract Turbulent diffusion with chemical reactions is of practical importance in many engineering and environmental
More information$arrow$ $\yen$ T (Yasutala Nagano) $arrow$ $\yen$ ?,,?,., (1),, (, ).,, $\langle$2),, (3),.., (4),,,., CFD ( ),,., CFD,.,,,
892 1995 105-116 105 $arrow$ $\yen$ T (Yasutala Nagano) $arrow$ $\yen$ - 1 7?,,?,, (1),, (, ),, $\langle$2),, (3),, (4),,,, CFD ( ),,, CFD,,,,,,,,, (3), $\overline{uv}$ 106 (a) (b) $=$ 1 - (5), 2,,,,,
More informationMD $\text{ }$ (Satoshi Yukawa)* (Nobuyasu Ito) Department of Applied Physics, School of Engineering, The University of Tokyo Lennar
1413 2005 36-44 36 MD $\text{ }$ (Satoshi Yukawa)* (Nobuyasu Ito) Department of Applied Physics, School of Engineering, The University of Tokyo Lennard-Jones [2] % 1 ( ) *yukawa@ap.t.u-tokyo.ac.jp ( )
More information40 $\mathrm{e}\mathrm{p}\mathrm{r}$ 45
ro 980 1997 44-55 44 $\mathrm{i}\mathrm{c}\mathrm{h}\mathrm{i}$ $-$ (Ko Ma $\iota_{\mathrm{s}\mathrm{u}\mathrm{n}}0$ ) $-$. $-$ $-$ $-$ $-$ $-$ $-$ 40 $\mathrm{e}\mathrm{p}\mathrm{r}$ 45 46 $-$. $\backslash
More informationMicrosoft Word - 158前刷.doc
既燃ガスに進入する未燃予混合気の燃焼について Combustion of unburnt gas mixture penetrating into burnt gas 溝渕泰寛, JAXA/ARD, 東京都調布市深大寺東町 7-44-1, mizo@chofu.jaxa.jp 竹野忠夫, JAXA/ARD, 東京都調布市深大寺東町 7-44-1 松山新吾, JAXA/ARD, 東京都調布市深大寺東町
More information[15] 1970 Chiu [16, 17] [18-22] [20] Chiu [23] [24] [25] Chiu [16, 17] Chiu G 2
Spray Combustion. Droplet Group Combustion 1. ml 20 µm 2.4 [1-12] [13] [14] 1 [15] 1970 Chiu [16, 17] [18-22] [20] Chiu [23] [24] 2. 2-1. [25] Chiu [16, 17] Chiu G 2 N: TOTAL NUMBER OF DROPLETS 9 8 7 6
More information110 $\ovalbox{\tt\small REJECT}^{\mathrm{i}}1W^{\mathrm{p}}\mathrm{n}$ 2 DDS 2 $(\mathrm{i}\mathrm{y}\mu \mathrm{i})$ $(\mathrm{m}\mathrm{i})$ 2
1539 2007 109-119 109 DDS (Drug Deltvery System) (Osamu Sano) $\mathrm{r}^{\mathrm{a}_{w^{1}}}$ $\mathrm{i}\mathrm{h}$ 1* ] $\dot{n}$ $\mathrm{a}g\mathrm{i}$ Td (Yisaku Nag$) JST CREST 1 ( ) DDS ($\mathrm{m}_{\mathrm{u}\mathrm{g}}\propto
More information音響問題における差分法を用いたインパルス応答解析予測手法の検討 (非線形波動現象の数理と応用)
1701 2010 72-81 72 Impulse Response Prediction for Acoustic Problem by FDM ( ), ) TSURU, Hideo (Nittobo Acoustic Engineering Co. Ltd.) IWATSU, Reima(Tokyo Denki University) ABSTRACT: The impulse response
More information,,, 2 ( ), $[2, 4]$, $[21, 25]$, $V$,, 31, 2, $V$, $V$ $V$, 2, (b) $-$,,, (1) : (2) : (3) : $r$ $R$ $r/r$, (4) : 3
1084 1999 124-134 124 3 1 (SUGIHARA Kokichi),,,,, 1, [5, 11, 12, 13], (2, 3 ), -,,,, 2 [5], 3,, 3, 2 2, -, 3,, 1,, 3 2,,, 3 $R$ ( ), $R$ $R$ $V$, $V$ $R$,,,, 3 2 125 1 3,,, 2 ( ), $[2, 4]$, $[21, 25]$,
More information316 on One Hundred Years of Boundary Layer Research, Proceedings of the IUTAM Symposium held at DLR-Göttingen, Germany, 2004, (eds. G. E. A. Meier and
316 on One Hundred Years of Boundary Layer Research, Proceedings of the IUTAM Symposium held at DLR-Göttingen, Germany, 2004, (eds. G. E. A. Meier and K. R. Sreenivasan), Solid Mech. Appl., 129, Springer,
More information広報さがみはら第1242号
LINE UP 3 1 5 6 1 NO.1242 S A G A M I H A R A 1 1 1 16 16 1 6 1 6 1 6 1 1 1 1 1 11 1 1 1 1 1 1 6 1 6 1 1 1 1 1 1 1 1 11 1 1 16 1 1 1 6 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 6 1 16 1 16 1 6 1 1 1 1 1 1
More information福岡大学人文論叢47-3
679 pp. 1 680 2 681 pp. 3 682 4 683 5 684 pp. 6 685 7 686 8 687 9 688 pp. b 10 689 11 690 12 691 13 692 pp. 14 693 15 694 a b 16 695 a b 17 696 a 18 697 B 19 698 A B B B A B B A A 20 699 pp. 21 700 pp.
More information$/\mathrm{t}\mathrm{a}\mathrm{k}\mathrm{a}\mathrm{y}\mathrm{a}$ MIYANO E mail: hirosaki-u.ac.jp 1 ( ) ( ) 1980
Title 非線形時系列解析によるカオス性検定 ( 非線形解析学と凸解析学の研究 ) Author(s) 宮野, 尚哉 Citation 数理解析研究所講究録 (2000), 1136: 28-36 Issue Date 2000-04 URL http://hdl.handle.net/2433/63786 Right Type Departmental Bulletin Paper Textversion
More informationEffects of Pressure on Unstretched Laminar Burning Velocity, Markstein Length and Cellularity of Propagating Spherical Laminar Flames Toshiaki KITAGAW
Effects of Pressure on Unstretched Laminar Burning Velocity, Markstein Length and Cellularity of Propagating Spherical Laminar Flames Toshiaki KITAGAWA*5, Yoshitaka TOGAMI, Kouji HARADA and Tomomi OGAWA
More information原著_十河.indd
51 156 2009 134-141 Journal of the Combustion Society of Japan Vol.51 No.156 (2009) 134-141 ORIGINAL PAPER 逆火限界付近における層流火炎基部の局所燃焼速度に与えるバーナ温度の影響 Influence of Burner Temperature on Local Burning Velocity
More information溝乱流における外層の乱れの巨視的構造に関するモデル Titleシミュレーション ( 乱れの発生, 維持機構および統計法則の数理 ) Author(s) 奥田, 貢 ; 辻本, 公一 ; 三宅, 裕 Citation 数理解析研究所講究録 (2002), 1285: Issue Date
溝乱流における外層の乱れの巨視的構造に関するモデル Titleシミュレーション ( 乱れの発生, 維持機構および統計法則の数理 ) Author(s) 奥田, 貢 ; 辻本, 公一 ; 三宅, 裕 Citation 数理解析研究所講究録 (2002), 1285: 92-99 Issue Date 2002-09 URL http://hdl.handle.net/2433/42433 Right
More information$\mathrm{v}$ ( )* $*1$ $\ovalbox{\tt\small REJECT}*2$ \searrow $\mathrm{b}$ $*3$ $*4$ ( ) [1] $*5$ $\mathrm{a}\mathrm{c}
Title 狩野本 綴術算経 について ( 数学史の研究 ) Author(s) 小川 束 Citation 数理解析研究所講究録 (2004) 1392: 60-68 Issue Date 2004-09 URL http://hdlhandlenet/2433/25859 Right Type Departmental Bulletin Paper Textversion publisher Kyoto
More informationJournal of the Combustion Society of Japan Vol.58 No.185 (2016) ORIGINAL PAPER 火災旋風近傍の流れに関する研究 Flow Around a Fire Whirl *
58 185 2016 167-171 Journal of the Combustion Society of Japan Vol.58 No.185 (2016) 167-171 ORIGINAL PAPER 火災旋風近傍の流れに関する研究 Flow Around a Fire Whirl * ONISHI, Hiroyuki and KUWANA, Kazunori 992-8510 4-3-16
More information工学的な設計のための流れと熱の数値シミュレーション
247 Introduction of Computational Simulation Methods of Flow and Heat Transfer for Engineering Design Minoru SHIRAZAKI Masako IWATA Ryutaro HIMENO PC CAD CAD 248 Voxel CAD Navier-Stokes v 1 + ( v ) v =
More information1 1 Emmons (1) 2 (2) 102
1075 1999 101-116 101 (Yutaka Miyake) 1. ( ) 1 1 Emmons (1) 2 (2) 102 103 1 2 ( ) : $w/r\omega$ $\text{ }$ 104 (3) $ $ $=-$ 2- - $\mathrm{n}$ 2. $\xi_{1}(=\xi),$ $\xi 2(=\eta),$ $\xi 3(=()$ $x,$ $y,$ $z$
More information$\Downarrow$ $\Downarrow$ Cahn-Hilliard (Daisuke Furihata) (Tomohiko Onda) 1 (Masatake Mori) Cahn-Hilliard Cahn-Hilliard ( ) $[1]^{1
$\Downarrow$ $\Downarrow$ 812 1992 67-93 67 Cahn-Hilliard (Daisuke Furihata (Tomohiko Onda 1 (Masatake Mori Cahn-Hilliard Cahn-Hilliard ( $[1]^{1}$ reduce ( Cahn-Hilliard ( Cahn- Hilliard Cahn-Hilliard
More informationTitle Compactification theorems in dimens Topology and Related Problems) Author(s) 木村, 孝 Citation 数理解析研究所講究録 (1996), 953: Issue Date URL
Title Compactification theorems in dimens Topology and Related Problems Authors 木村 孝 Citation 数理解析研究所講究録 1996 953 73-92 Issue Date 1996-06 URL http//hdlhandlenet/2433/60394 Right Type Departmental Bulletin
More informationTitle 半線形波動方程式系の解の爆発 ( 非線型双曲型方程式系の解の挙動に関する研究 ) Author(s) 太田, 雅人 Citation 数理解析研究所講究録 (2003), 1331: Issue Date URL
Title 半線形波動方程式系の解の爆発 ( 非線型双曲型方程式系の解の挙動に関する研究 ) Author(s) 太田 雅人 Citation 数理解析研究所講究録 (2003) 1331: 34-49 Issue Date 2003-07 URL http://hdlhandlenet/2433/43289 Right Type Departmental Bulletin Paper Textversion
More informationArchimedean Spiral 1, ( ) Archimedean Spiral Archimedean Spiral ( $\mathrm{b}.\mathrm{c}$ ) 1 P $P$ 1) Spiral S
Title 初期和算にみる Archimedean Spiral について ( 数学究 ) Author(s) 小林, 龍彦 Citation 数理解析研究所講究録 (2000), 1130: 220-228 Issue Date 2000-02 URL http://hdl.handle.net/2433/63667 Right Type Departmental Bulletin Paper Textversion
More informationTitle 非線形シュレディンガー方程式に対する3 次分散項の効果 ( 流体における波動現象の数理とその応用 ) Author(s) 及川, 正行 Citation 数理解析研究所講究録 (1993), 830: Issue Date URL
Title 非線形シュレディンガー方程式に対する3 次分散項の効果 ( 流体における波動現象の数理とその応用 ) Author(s) 及川 正行 Citation 数理解析研究所講究録 (1993) 830: 244-253 Issue Date 1993-04 URL http://hdlhandlenet/2433/83338 Right Type Departmental Bulletin Paper
More information空力騒音シミュレータの開発
41 COSMOS-V, an Aerodynamic Noise Simulator Nariaki Horinouchi COSMOS-V COSMOS-V COSMOS-V 3 The present and future computational problems of the aerodynamic noise analysis using COSMOS-V, our in-house
More informationmains.dvi
8 Λ MRI.COM 8.1 Mellor and Yamada (198) level.5 8. Noh and Kim (1999) 8.3 Large et al. (1994) K-profile parameterization 8.1 8.1: (MRI.COM ) Mellor and Yamada Noh and Kim KPP (avdsl) K H K B K x (avm)
More information1 10 500 67 [7,8] 1995 9 ([2]) [cm/s] 1 1 Ω i (i = 1, 2, 3, 4, 5) 1: Geological features and permeability coefficient ([2]) (cm/s) Ω 1 6.72 10 4 Ω 3 1
Numerical method by use of color digital images and its application to underground water flow through industrial waste in Teshima Island. 1 2 Takako Yoshii 1 and Hideyuki Koshigoe 2 Graduate School of
More information(Koji Kawasaki) Department of Civil Engineering, Graduate School of Engineering Nagoya University 1.,.,,,,,.,,,,,,,.,,,,.,,,,., (19
1673 2010 77-92 77 (Koji Kawasaki) Department of Civil Engineering, Graduate School of Engineering Nagoya University 1,,,,,,,,,,,,,,,,,,,,,, (1996 1999) $\sim$ VOF (Volume OfFluid), CADMAS-SURF (SUper
More information\mathrm{n}\circ$) (Tohru $\mathrm{o}\mathrm{k}\mathrm{u}\mathrm{z}\circ 1 $(\mathrm{f}_{\circ \mathrm{a}}\mathrm{m})$ ( ) ( ). - $\
1081 1999 84-99 84 \mathrm{n}\circ$) (Tohru $\mathrm{o}\mathrm{k}\mathrm{u}\mathrm{z}\circ 1 $(\mathrm{f}_{\circ \mathrm{a}}\mathrm{m})$ ( ) ( ) - $\text{ }$ 2 2 ( ) $\mathrm{c}$ 85 $\text{ }$ 3 ( 4 )
More information2 q effective mean dynamic pressure [Pa] q cr critical value of dynamic pressure [Pa] q CW heat flux for cold wall [J/m 2 ] r th throat radius [m] x a
1 1 2 3 4 5 6 Estimation of Recession Amount of Nozzle Wall using Coupled Fluid/Thermochemical Approach by Yu DAIMON* 1, Toru SHIMADA* 2, Nobuyuki TSUBOI* 3, Ryoji TAKAKI* 4, Kazuhisa FUJITA* 5 and Kuniyuki
More information空間多次元 Navier-Stokes 方程式に対する無反射境界条件
81 Navier-Stokes Poinsot Lele Poinsot Lele Thompson Euler Navier-Stokes A Characteristic Nonreflecting Boundary Condition for the Multidimensional Navier-Stokes Equations Takaharu YAGUCHI, Kokichi SUGIHARA
More information$\mathrm{c}_{j}$ $u$ $u$ 1: (a) (b) (c) $y$ ($y=0$ ) (a) (c) $i$ (soft-sphere) ( $m$:(mj) $\sigma$:(\sigma j) $i$ $(r_{1j}.$ $j$ $r_{i}$ $r_{j}$ $=r:-
1413 2005 60-69 60 (Namiko Mitarai) Frontier Research System, RIKEN (Hiizu Nakanishi) Department of Physics, Faculty of Science, Kyushu University 1 : [1] $[2, 3]$ 1 $[3, 4]$.$\text{ }$ [5] 2 (collisional
More information$\sim 22$ *) 1 $(2R)_{\text{}}$ $(2r)_{\text{}}$ 1 1 $(a)$ $(S)_{\text{}}$ $(L)$ 1 ( ) ( 2:1712 ) 3 ( ) 1) 2 18 ( 13 :
Title 角術への三角法の応用について ( 数学史の研究 ) Author(s) 小林, 龍彦 Citation 数理解析研究所講究録 (2001), 1195: 165-175 Issue Date 2001-04 URL http://hdl.handle.net/2433/64832 Right Type Departmental Bulletin Paper Textversion publisher
More informationTitle ゾウリムシの生物対流実験 ( 複雑流体の数理とその応用 ) Author(s) 狐崎, 創 ; 小森, 理絵 ; 春本, 晃江 Citation 数理解析研究所講究録 (2006), 1472: Issue Date URL
Title ゾウリムシの生物対流実験 ( 複雑流体の数理とその応用 ) Author(s) 狐崎, 創 ; 小森, 理絵 ; 春本, 晃江 Citation 数理解析研究所講究録 (2006), 1472: 129-138 Issue Date 2006-02 URL http://hdl.handle.net/2433/48126 Right Type Departmental Bulletin
More informationFig. 2 Pressure-temperature diagram of pure substance and mixed thel consisting of n-tridecane and n-pentane Fig. 1 Schematic of present model
Cavitation Induced Breakup Model for Multicomponent Fuel Spray Authors have developed a spray model for multicomponent fuel and reported the successful model which represents batch-distillation in multicomponent
More information76 20 ( ) (Matteo Ricci ) Clavius 34 (1606) 1607 Clavius (1720) ( ) 4 ( ) \sim... ( 2 (1855) $-$ 6 (1917)) 2 (1866) $-4$ (1868)
$\mathrm{p}_{\mathrm{r}\mathrm{o}\mathrm{g}\mathrm{r}\mathrm{a}}\mathrm{m}\dagger 1$ 1064 1998 75-91 75 $-$ $\text{ }$ (Osamu Kota) ( ) (1) (2) (3) 1. 5 (1872) 5 $ \mathrm{e}t\mathrm{l}\mathrm{a}\mathrm{n}\mathrm{g}\mathrm{e}\mathrm{r}$
More informationNUMERICAL CALCULATION OF TURBULENT OPEN-CHANNEL FLOWS BY USING A MODIFIED /g-e TURBULENCE MODEL By Iehisa NEZU and Hiroji NAKAGA WA Numerical calculat
NUMERICAL CALCULATION OF TURBULENT OPEN-CHANNEL FLOWS BY USING A MODIFIED /g-e TURBULENCE MODEL By Iehisa NEZU and Hiroji NAKAGA WA Numerical calculation techniques of turbulent shear flows are classified
More informationFig. 1 Experimental apparatus.
Effects of Concentration of Surfactant Solutions on Drag-Reducing Turbulent Boundary Layer In this study, the influence of a drag-reducing surfactant on the turbulent boundary layer was extensively investigated
More information,.,.,,. [15],.,.,,., 2003 3 2006 2 3. 2003 3 2004 2 2004 3 2005 2, 1., 2005 3 2006 2, 1., 1,., 1,,., 1. i
200520866 ( ) 19 1 ,.,.,,. [15],.,.,,., 2003 3 2006 2 3. 2003 3 2004 2 2004 3 2005 2, 1., 2005 3 2006 2, 1., 1,., 1,,., 1. i 1 1 1.1..................................... 1 1.2...................................
More information14 6. $P179$ 1984 r ( 2 $arrow$ $arrow$ F 7. $P181$ 2011 f ( 1 418[? [ 8. $P243$ ( $\cdot P260$ 2824 F ( 1 151? 10. $P292
1130 2000 13-28 13 USJC (Yasukuni Shimoura I. [ ]. ( 56 1. 78 $0753$ [ ( 1 352[ 2. 78 $0754$ [ ( 1 348 3. 88 $0880$ F ( 3 422 4. 93 $0942$ 1 ( ( 1 5. $P121$ 1281 F ( 1 278 [ 14 6. $P179$ 1984 r ( 2 $arrow$
More information$\mathbb{h}_{1}^{3}(-c^{2})$ 12 $([\mathrm{a}\mathrm{a}1 [\mathrm{a}\mathrm{a}3])$ CMC Kenmotsu-Bryant CMC $\mathrm{l}^{3}$ Minkowski $H(\neq 0)$ Kenm
995 1997 11-27 11 3 3 Euclid (Reiko Aiyama) (Kazuo Akutagawa) (CMC) $H$ ( ) $H=0$ ( ) Weierstrass $g$ 1 $H\neq 0$ Kenmotsu $([\mathrm{k}])$ $\mathrm{s}^{2}$ 2 $g$ CMC $P$ $([\mathrm{b}])$ $g$ Gauss Bryant
More information) [9] DNS DNS Westbrook and Dryer[10] ( ) [11] DNS Markstein Markstein Markstein Markstein Markstein [12,13] Markstein Markstein Marks
56 177 2014 251-257 Journal of the Combustion Society of Japan Vol.56 No.177 (2014) 251-257 ORIGINAL PAPER 爆発シミュレーションに特化した水素 空気系の総括反応モデルに関する理論的検討 Theoretical Analysis of Global Reaction Model of H 2 /air
More information第86回日本感染症学会総会学術集会後抄録(II)
χ μ μ μ μ β β μ μ μ μ β μ μ μ β β β α β β β λ Ι β μ μ β Δ Δ Δ Δ Δ μ μ α φ φ φ α γ φ φ γ φ φ γ γδ φ γδ γ φ φ φ φ φ φ φ φ φ φ φ φ φ α γ γ γ α α α α α γ γ γ γ γ γ γ α γ α γ γ μ μ κ κ α α α β α
More informationTitle DEA ゲームの凸性 ( 数理最適化から見た 凸性の深み, 非凸性の魅惑 ) Author(s) 中林, 健 ; 刀根, 薫 Citation 数理解析研究所講究録 (2004), 1349: Issue Date URL
Title DEA ゲームの凸性 ( 数理最適化から見た 凸性の深み 非凸性の魅惑 ) Author(s) 中林 健 ; 刀根 薫 Citation 数理解析研究所講究録 (2004) 1349: 204-220 Issue Date 2004-01 URL http://hdl.handle.net/2433/24871 Right Type Departmental Bulletin Paper
More information$\ovalbox{\tt\small REJECT}$ SDE 1 1 SDE ;1) SDE 2) Burgers Model SDE $([4],[5],[7], [8])$ 1.1 SDE SDE (cf.[4],[5]) SDE $\{$ : $dx_
$\ovalbox{\tt\small REJECT}$ 1032 1998 46-61 46 SDE 1 1 SDE ;1) SDE 2) Burgers Model SDE $([4],[5],[7], [8])$ 1.1 SDE SDE (cf.[4],[5]) SDE $dx_{t}=a(t, X_{t}, u)dt+b(t, x_{t}, u)dwt$, $X_{0}=\xi(\omega)$
More information(6) (111) (148) (129) (169) CAPCOM ANNUAL REPORT
62 63 65 69 71 72 73 74 91 61 CAPCOM ANNUAL REPORT 213 22 26 276 143 92 13 113 73 122 (6) (111) (148) (129) (169) 23 24 25 27 28 29 21 211 212 213 CAPCOM ANNUAL REPORT 213 62 63 CAPCOM ANNUAL REPORT 213
More information112 Landau Table 1 Poiseuille Rayleigh-Benard Rayleigh-Benard Figure 1; 3 19 Poiseuille $R_{c}^{-1}-R^{-1}$ $ z ^{2}$ 3 $\epsilon^{2}=r_{\mathrm{c}}^{
1454 2005 111-124 111 Rayleigh-Benard (Kaoru Fujimura) Department of Appiied Mathematics and Physics Tottori University 1 Euclid Rayleigh-B\ enard Marangoni 6 4 6 4 ( ) 3 Boussinesq 1 Rayleigh-Benard Boussinesq
More informationReport of Special Research from the National Institute for Environmental Studies, Japan NATIONAL INSTITUTE FOR ENVIRONMENTAL STUDIES
Report of Special Research from the National Institute for Environmental Studies, Japan NATIONAL INSTITUTE FOR ENVIRONMENTAL STUDIES ) V O Cvolatile organic compounds V O C V O C 1940 10 1 1 N Ox V
More information(PML) Perfectly Matched Layer for Numerical Method in Unbounded Region ( ( M2) ) 1,.., $\mathrm{d}\mathrm{t}\mathrm{n}$,.,, Diri
1441 25 187-197 187 (PML) Perfectly Matched Layer for Numerical Method in Unbounded Region ( ( M2) ) 1 $\mathrm{d}\mathrm{t}\mathrm{n}$ Dirichlet Neumann Neumann Neumann (-1) ([6] [12] ) $\llcorner$ $\langle$
More information,, Mellor 1973),, Mellor and Yamada 1974) Mellor 1973), Mellor and Yamada 1974) 4 2 3, 2 4,
Mellor and Yamada1974) The Turbulence Closure Model of Mellor and Yamada 1974) Kitamori Taichi 2004/01/30 ,, Mellor 1973),, Mellor and Yamada 1974) Mellor 1973), 4 1 4 Mellor and Yamada 1974) 4 2 3, 2
More information$\mathrm{i}\mathrm{d}$ 15 ) Authorization ( ) Accounting ( ) UNIX Authentication ID Authorization Accounting $\sim-$ UNIX Authentication BSD Flat Data
2})$ $ \ulcorner^{-}$ 1446 2005 14-39 14 Central Authentication and Authorization Service -Web Applicatim - (Hisashi NAITO) (Shoji KAJITA) Graduate School of Mathematics Information Technology Center Nagoya
More information(Nobumasa SUGIMOTO) (Masatomi YOSHIDA) Graduate School of Engineering Science, Osaka University 1., [1].,., 30 (Rott),.,,,. [2].
1483 2006 112-121 112 (Nobumasa SUGIMOTO) (Masatomi YOSHIDA) Graduate School of Engineering Science Osaka University 1 [1] 30 (Rott) [2] $-1/2$ [3] [4] -\mbox{\boldmath $\pi$}/4 - \mbox{\boldmath $\pi$}/2
More informationA MATLAB Toolbox for Parametric Rob TitleDesign based on symbolic computatio Design of Algorithms, Implementatio Author(s) 坂部, 啓 ; 屋並, 仁史 ; 穴井, 宏和 ; 原
A MATLAB Toolbox for Parametric Rob TitleDesign based on symbolic computatio Design of Algorithms, Implementatio Author(s) 坂部, 啓 ; 屋並, 仁史 ; 穴井, 宏和 ; 原, 辰次 Citation 数理解析研究所講究録 (2004), 1395: 231-237 Issue
More information『赤すぐ』『妊すぐ』<出産・育児トレンド調査2003>
79.9 1.6 UP 86.6% 7.0 UP 61.3% 12.7UP 18-24 3 66.6 3.0 UP 38.7 0.7 UP 14.8 1.9 UP 13.3 0.3UP 4 1 024 1.23 0.01down Topics 5 79.9 1.6UP 7.0 UP 12.7U 3.5 0.4 UP 3.4 0.4 UP 6 73.1% 5.7 UP 75.0% 71.2% 7 53.9%
More informationuntitled
10 log 10 W W 10 L W = 10 log 10 W 10 12 10 log 10 I I 0 I 0 =10 12 I = P2 ρc = ρcv2 L p = 10 log 10 p 2 p 0 2 = 20 log 10 p p = 20 log p 10 0 2 10 5 L 3 = 10 log 10 10 L 1 /10 +10 L 2 ( /10 ) L 1 =10
More information2 (March 13, 2010) N Λ a = i,j=1 x i ( d (a) i,j x j ), Λ h = N i,j=1 x i ( d (h) i,j x j ) B a B h B a = N i,j=1 ν i d (a) i,j, B h = x j N i,j=1 ν i
1. A. M. Turing [18] 60 Turing A. Gierer H. Meinhardt [1] : (GM) ) a t = D a a xx µa + ρ (c a2 h + ρ 0 (0 < x < l, t > 0) h t = D h h xx νh + c ρ a 2 (0 < x < l, t > 0) a x = h x = 0 (x = 0, l) a = a(x,
More information7 OpenFOAM 6) OpenFOAM (Fujitsu PRIMERGY BX9, TFLOPS) Fluent 8) ( ) 9, 1) 11 13) OpenFOAM - realizable k-ε 1) Launder-Gibson 15) OpenFOAM 1.6 CFD ( )
71 特集 オープンソースの大きな流れ Nonlinear Sloshing Analysis in a Three-dimensional Rectangular Pool Ken UZAWA, The Center for Computational Sciences and E-systems, Japan Atomic Energy Agency 1 1.1 ( ) (RIST) (ORNL/RSICC)
More information1 食品安全を主な目的とする取組
--a 2003 7 26 3. 3.1-1- 16 2 27 0227012-2-a 23 7 1 82 2 1 7 9 2 ( ) -2- -2-b 19 3 28 18 14701-2-c ) 15 5 2-3- 26 21 7 2 2 7 2 3 7 2 4 10 83 23 3 1 7 2 5 7 2 5-2-d -4- -5 - -3-a -6- -4-a -7- -4-b -8- -5-a
More information2
2 3 Page 4 5 6 A-1B-1 C0 D0 E0 F0 G0 A0 B0 C1 D1 E1 F1 G1 A1 B1 C2 D2 E2 F2 G2 A2 B2 C3 D3 E3 7 F3 G3 A3 B3 C4 D4 E4 F4 G4 A4 B4 C5 D5 E5 F5 G5 A5 B5 C6 D6 E6 F6 G6 A6 B6 C7 8 Page 9 1 2 3 1 2 10 1 11
More information% 32.3 DI DI
2011 7 9 28.1 41.4 30.5 35.8 31.9% 32.3 DI 18.2 2.4 8.1 3.5 DI 9.4 32.2 0.0 25.9 2008 1 3 2 3 34.8 65.2 46.753.8 1 2 8.82.9 43.1 10 3 DI 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25
More information31, 21% 24, 17% 8, 5% 23, 16% 24, 16% 91, 62% 19, 13% 39, 27% 33, 23% 73 48 57 51 31 1 9 13.0% 7.4% 5.3% 12.5% 17.1% 13.2% 17.9% 4.5% 36.4% 56.5% 40.7% 36.8% 50.0% 67.1% 56.3% 65.8% 75.0% 26.0% 37.0%
More information2 DI 28 7 1 37 28 4 18 27 11 21 5 2 26 4 5 1 15 2 25 3 35 4 17 7 5 48 76 31 47 17 2 92 12 2 2 4 6 8 1 12 1 2 4 1 12 13 18 19 3 42 57 57 1 2 3 4 5 6 1 1 1 3 4 4 5 5 5.5 1 1.5 2 2.5 3 3.5 4 4.5 5
More information37 27.0% 26 19.0% 74 54.0% 9 6.4% 13 9.2% 28 19.9% 26 18.4% 37 26.2%. 24 17.0% 99 69 75 59 39 1 6 4.5% 1.4% 7.7% 2.9% 25.0% 17.9% 20.8% 50.0% 41.7% 47.0% 51.4% 54.3% 61.5% 57.1% 55.6% 42.4% 50.0% 58.3%
More information3 DI 29 7 1 5 6 575 11 751, 13 1,1,25 6 1,251,5 2 1,51,75 1,752, 1 2,2,25 2,252,5 2,53, 3,3,5 3,5 5 1 15 2 25 3 5 6 575 12 751, 21 1,1,25 27 1,251,5 9 1,51,75 1,752, 1 2,2,25 2 2,252,5 2,53, 2 3,3,5
More information„´™Ÿ/’£flö
48 144 2006 206-213 Journal of the Combustion Society of Japan Vol. 48 No. 144 (2006) 206-213 ORGNAL PAPER * * An Approach to Combustion Diagnostics of Premixed Flame by Chemiluminescence of OH * and CH
More informationA03-2.dvi
14 A3-2 Numerical Analyses in the Secondary Combustion Chamber of the Ducted Rocket Engine 184-8588 2-24-16 E-mail: kikumoto@starcadmechtuatacjp Kousuke KIKUMOTO Dept of Mech Systems Eng Tokyo Noko Univ
More informationカルマン渦列の消滅と再生成のメカニズム
1822 2013 97-108 97 (Jiro Mizushima) (Hiroshi Akamine) Department of Mechanical Engineering, Doshisha University 1. [1,2]. Taneda[3] Taneda 100 ( d) $50d\sim 100d$ $100d$ Taneda Durgin and Karlsson[4]
More informationD v D F v/d F v D F η v D (3.2) (a) F=0 (b) v=const. D F v Newtonian fluid σ ė σ = ηė (2.2) ė kl σ ij = D ijkl ė kl D ijkl (2.14) ė ij (3.3) µ η visco
post glacial rebound 3.1 Viscosity and Newtonian fluid f i = kx i σ ij e kl ideal fluid (1.9) irreversible process e ij u k strain rate tensor (3.1) v i u i / t e ij v F 23 D v D F v/d F v D F η v D (3.2)
More information