42 EGR R egr - f (p i , N e , F egr ) 102, 3, 6, 74 43 NOx_flow ṁ nox - C nox 50 e (-R resf * 12.88) 7.955 x 10 -6 P imep b 2 s π /4 n c N e /7122 44 Tm<strong>an</strong>ifold T m - (310 + R egr 400) / (1 + R egr /100) 105, 102 45 Residual R resf - f (R egr , p i ) 119, 102, 3 121, 119, 6, 76, 77, 82, 109 46 Burn_rate θ 0-90 - F(N e , b, s, R resf ,R af , p i , T m ) 3, 6, 75, 76, 77, 103, 105., 119 47 Nstall N stall - K o T i -0.5 . 70, 64, 17 48 GB_effic η gb - f (T gb , N t, i gear ) 47, 18, 8, 53 49 Tchurning Tch - f (Nt, i_gear) 20, 8, 53 50 Gear_state i gear - f(p i, N t ) 53, 3, 8 51 Gear_ratio ξ gb - f (i gear , ξ 1 , ξ 2 , ξ 3 , ξ 4 ) 48, 53, 58, 59, 60, 50 52 Gear_sp<strong>an</strong> ξ sp<strong>an</strong> - ξ 1 /ξ 4 49, 50, 58 53 Stall_capac K o - K obase α t 1.7 64, 61 54 Stall_ratio R to - R obase α t 66, 61 55 TC-capac K(R s , K o ) - N e T -0.5 i 65,15 ,64 ,6 ,17 56 TC_ratio R t (R s , R to ) - T t /Τ i 67, 66, 15, 71,17 57 Dc D c = D cbase α t -0.68 69, 61 58 f ṁ f 120, 3,105,6,82,76,77,103 59 g1 ṁ nox ηcat 0,121, 119, 16, 6, 60 g2 f (dV/dt,) 34,2,22,29,31,28,46 61 g3 f(dV/dt) 34,22,22,29,31,28,46 62 g4 f(dV/dt) 34,22,22,29,31,28,46 63 g5 sin αs-(Te(60 ξfd ξ1Vs/(2 re π)) ξfd ξ1 ηfdηgb Rto - re (Froll + Faero)) (re M g) -1 24, 16, 55, 58, 42, 54, 47, 66, 29, 28, 34 64 g6 sin αc - (Te(60 ξfd ξ4 Vc/(2 re π)) ξfd ξ4 ηfdηgb - re (Froll + Faero)) (re M g) -1 25, 16, 55, 50, 42,, 54, 47, 29, 28, 34 65 g7 T e (N e )/T elug (N e ) -1 16, 6
66 67 68 69 70 71 72 73 74 75 76 77 78 79 80 81 82 83 84 85 86 g8 c r - 13.2 + 0.045 b 78, 76 g9 θ 0−90 − 70 75 g12 1.6 - ξ 1 / ξ 2 58, 59 g13 ξ 1 / ξ 2 - 2. 58, 59 g14 1.2 - ξ 2 / ξ 3 59, 60 g15 ξ 2 / ξ 3 - 1.6 59, 60 g16 3.5- ξ 1 / ξ 4 58, 50 g17 ξ 1 / ξ 4 - 4.5 58, 50 g18 0.8 - b/s 76, 77 g19 b/s - 1.2 76, 77 g20 g21 400 - π b 2 s/ (4 n c ) x 10 -3 76, 77, 82 π b 2 s/ (4 n c ) x 10 -3 - 600 76, 77, 82 g22 d i + d e -.88 b 79, 80 g23 0.85 - d e /d i 79,.80 g24 d e /d i - 0.87 79, 80 g25 i vo -e vc - 40 84, 85 g26 acc iv ( i vo i vc i lift ) - K acci 83, 84, 87 g27 acc ev ( e vo e vc e lift ) - K acce 85, 86, 88 h1 d bm /b - K dm 92, 76 h2 l bm / b - K lm 93, 76 h3 d br / b - K dr 90, 76 h4 l br / b - K lr 91, 76
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UNIVERSITY OF MICHIGAN DEPARTMENT O
- Page 3 and 4: epresentation facilitates decomposi
- Page 5 and 6: of changes in these parameters on t
- Page 7 and 8: The U.S. metro-highway fuel economy
- Page 9 and 10: Powertrain Relationships The princi
- Page 11 and 12: N ds = ξ fd N d (23) dN ds /dt =
- Page 13 and 14: to be stalled (Rs = 0). Equation (3
- Page 15 and 16: the surface-to-volume ratio at a vo
- Page 17 and 18: intake and exhaust valve, and acros
- Page 19 and 20: driveability. These values are stor
- Page 21 and 22: τ dV τ 0-60 = τ :⌡ ⌠ dt dt =
- Page 23 and 24: There are also several geometric co
- Page 25 and 26: g 13 : ξ 1 / ξ 2 - 2.0 ≤ 0 Step
- Page 27 and 28: x 2 h 2 (y, x 2 ) = 0 h 2 ( x 2 )=
- Page 29 and 30: Master Problem Subproblem min f(y,
- Page 31 and 32: 6 COORDINATED OPTIMIZATION SOLUTION
- Page 33 and 34: educes fuel flow by 1.3%; the const
- Page 35 and 36: Assanis, D.N., and Polishak, M. 198
- Page 37 and 38: Patton, K.J., Nitschke, R.G., and H
- Page 39 and 40: DECOMPOSITION ANALYSIS MODEL -BASED
- Page 41 and 42: Master Problem Subproblem (i = 1, .
- Page 43 and 44: 1 2 Impeller Stator Vortex flow dir
- Page 45 and 46: Partitioned Graph Resultant FDT 111
- Page 47 and 48: Table I Summary of Coordination Str
- Page 49 and 50: Index Variable Partition Descriptio
- Page 51 and 52: Index Variable Partition Descriptio
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- Page 61 and 62: Table B.8: Accessory losses. Amps @