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Vozila i delovi chevron_right Delovi i oprema
Pločice za prednje kočnice Brembo P 23 136 garnitura 4 kom. Kočioni sistem brembo, sa električnim indikatorom istrošenosti. Zamenjuje Brembo P 61 093 WVA 24466, 24467 Citroen Jumper Box/Bus/Platform/Chassis (2000kg korisne nosivosti +visoka nosivost) 2.0 BlueHDi 110/130/130 4x4/160/160 4x4 / 2.2 HDi 100/110/120/130/150 / 3.0 HDi 145/155/160/180 04/06> Fiat Ducato Box/Bus/Platform/Chassis (2000kg korisne nosivosti) 115 Multijet 2,0 D / 100 Multijet 2,2 D / 110/120/130/150/180 Multijet 2,3 D / 120 Multijet 2,3 D 4x4 / 140 Natural Power / 150/160/180 Multijet 3,0 D 07/06> Peugeot Boxer Box/Bus/Platform/Chassis (2000kg korisne nosivosti +visoka nosivost) 2.0 BlueHDi 110/130/160 / 2.2 HDi 100/110/120/130/150 / 3.0 D / 3.0 HDi / 3.0 HDi 145/160/175 04/06> Detaljnije Brembo kataloški broj: P 23 136 OEM brojevi: 1612433780 77366023 77366024 77367090 Proizvođač: Brembo S.P.A. Italija Zemlja porekla: Italija Uvoznik: Sanel d.o.o. Beograd Nisu nađene recenzije Ocenite ovaj proizvod Podelite vaše utiske sa ostalim kupcima Napišite recenziju Proizvođač: Zemlja porekla:
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Vozila i delovi chevron_right Delovi i oprema
Pločice za prednje kočnice Brembo P 59 084 garnitura 4 kom. Kočioni sistem Teves, sa akustičnim indikatorom istrošenosti. WVA 22123, 22124 Opel Corsa E / Corsa E Van (točkovi 14") 1.0 / 1.2 / 1.3 CDTI / 1.4 / 1.4 LPG / 1.4 Turbo 09/14> Vauxhall Corsa E / Corsa E Van 08/14> Detaljnije Brembo kataloški broj: P 59 084 OEM brojevi: 1605280 95517028 Proizvođač: Brembo S.P.A. Italija Zemlja porekla: Italija Uvoznik: Sanel d.o.o. Beograd Nisu nađene recenzije Ocenite ovaj proizvod Podelite vaše utiske sa ostalim kupcima Napišite recenziju Proizvođač: Zemlja porekla:
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Vozila i delovi chevron_right Delovi i oprema
Pločice za prednje kočnice Brembo P 06 021 garnitura 4 kom. Kočioni sistem Teves, sa pripremom za indikator istrošenosti. WVA 21486, 21642 Alpina B10 / B10 Estate (E39) 4.6 V8 12/96>09/02 BMW 5 / 5 Touring (E39) 520 d / 520 i / 525 d / 525 i / 530 d / 530 i / 535 i / 540 i / M5 09/97>05/04, 7 (E38) 740 i/iL 10/94>11/01, X3 (E83) 3.0 sd / xDrive 35 d 09/06>08/11, X5 (E53) 3.0 d / 3.0 i / 4.4 i 05/00>12/06 Detaljnije Brembo kataloški broj: P 06 021 OEM brojevi: 34111163307 34111165227 34112157589 34112180419 34112229031 34112282165 34112282166 34112282556 34112357230 34113427503 34116761252 Proizvođač: Brembo S.P.A. Italija Zemlja porekla: Italija Uvoznik: Sanel d.o.o. Beograd Nisu nađene recenzije Ocenite ovaj proizvod Podelite vaše utiske sa ostalim kupcima Napišite recenziju Proizvođač: Zemlja porekla:
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Kolekcionarstvo i umetnost chevron_right Kolekcionarstvo
Par trosistemskih auto zvucnika Pružaju jasan, uravnotežen zvuk punog frekventnog opsega Dizajn koji štedi prostor i minimalna velicina pojednostavljuju instalaciju Serija WRX Tip Trosistemski Snaga 220 W (2x110 W) Frekventni opseg 45-20000 Hz Osetljivost 88 dB Impedansa 4 Ohm Niskotonac 165 mm PEI membrana Srednjotonac 30 mm "mylar" kalotni Visokotonac 15 mm piezo Vešanje Gumeno Materijal kucišta Aluminijum Velicina zvucnika 165 mm Ugradne dimenzije 145 mm (širina) x 63 mm (dubina) Par trosistemskih auto zvucnika Pružaju jasan, uravnotežen zvuk punog frekventnog opsega Dizajn koji štedi prostor i minimalna velicina pojednostavljuju instalaciju Serija WRX Tip Trosistemski Snaga 220 W (2x110 W) Frekventni opseg 45-20000 Hz Osetljivost 88 dB Impedansa 4 Ohm Niskotonac 165 mm PEI membrana Srednjotonac 30 mm "mylar" kalotni Visokotonac 15 mm piezo Vešanje Gumeno Materijal kucišta Aluminijum Velicina zvucnika 165 mm Ugradne dimenzije 145 mm (širina) x 63 mm (dubina)
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Kolekcionarstvo i umetnost chevron_right Kolekcionarstvo
77 znacaka: vojne škole, oznake jedinica, divizije i brigade.
58963) TRANSONIC AERODYNAMICS NUMERICAL ANALYSIS , Petrović Z. , Stupar S. , Mechanical Engineering Faculty University of Belgrade 1996 ; Contents : 1 Introduction 1.1 Preliminary Remarks. 1.2 Governing Equations 1.3 Simplifications to the Governing Equations 1.3.1 Definition of an Adiabatic Flow. 1.3.2 Definition of an Irrotational Flow 1.3.3 Crocco`s Theorem 1.3.4 Isentropic Gas Relation 1.4 Algebraic Form of Energy Equation for Steady Adiabatic Flow 1.5 The Isentropic Form of the Energy Equation 1.6 The Momentum Conservation Laws. 1.7 Isentropic Shocks vs. `Real World Shocks` 1.7.1 Rankine-Hugoniot approach 1.7.2 Isentropic approach 1.8 Techniques for Handling Shocks in Potential Flow Calculations 1.9 Summary 2 Transonic Small Disturbance Equation 2.1 Preliminary Remarks. 2.1.1 Treatment of Flow Angle of Attack 2.2 Definition of Disturbance Potential 2.3 Boundаry Conditions for Flow at the Body Surface 2.4 Derivation of the TSD Equation 2.5 Properties of the TSD Equation. 2.6 Finite Difference Terminology 2.7 Conservation Form vs. Non-Conservation Form 2.8 Finite Difference Expression Form of the TSD Equation in Subsoni 2.9 Murman-Cole Switching in supersonic Regions 2.10 Discretization Error Associated with Equation (2.2) 2.11 Loss of Conservation Property due to Switching 2.12 Murman-Cole Switching in Conservation Form 2.13 Application of Boundary Conditions 2.13.1 Region Ahead of the Leading Edge: (1 2.13.2 Region of the Slit: (ILE SITE) 2.13.3 Region Downstream of the Trailing Edge: (ITE << Imax 2.14 Far Field Boundary Conditions 2.15 Relaxation Procedure for the TSD Equation 2.15.1 Gauss-Seidel Scheme 2.16 The Point Successive Over-Relaxation (SOR) Scheme 2.17 The Line Gauss-Seidel Iteration Scheme 2.18 The Thomas Algorithm 2.19 Solution of the SLOR Scheme to TSD Equation 2.20 Summary 3 The Transonic Full Potential Equation 3.1 Introduction 3.2 Jameson`s Rotated Difference Scheme 3.3 Transformation of the Continuity Equation to a Curvilinear Coordina System. 3.4 Boundary Conditions. 3.4.1 Boundary Condition at the Solid Surface 3.4.2 Boundary Conditions at the Far Field... 3.5 Governing Equation for Axisymmetric Flows in the Transformed Plan 3.6 Construction of the Body-Fitted Coordinate system... 3.6.1 H-grid, algebraic approach 3.6.2 O-grid, algebraic approach. 3.7 Construction of C-Grids Around Airfoils 3.8 Generation of the Orthogonal Grid... 3.9 Discretization of the Governing Equation 3.10 Computation of Metrics at Half Points 3.11 Computation of Densities and Contravariant Velocities.. 3.12 Relaxation Procedure for Solving the Full Potential Equation 3.12.1 Interior Points 3.13 Summary 4 Numerical Technique for Designing Airfoils 4.1 Introduction. 4.2 Optimization Approach 4.2.1 Design Objective 4.2.2 Design Point 4.2.3 Starting Point. 4.2.4 Design Variables 4.2.5 Design Constraints 4.2.6 Black Box. 4.3 CONMIN to Black Box Coupling. 4.3.1 Optimization Process 4.4 Inverse Design Techniques. 4.5 Carlson`s Inverse Design Technique.. 5 Unsteady Transonic Potential Flow 5.1 Introduction. 5.2 Governing Equations 5.3 Unsteady Transonic Small Disturbance Equation 5.4 Boundary Conditions. 5.5 Low-Frequency Approximation 5.6 Characteristic of the Low-Frequency Transonic Small Disturbance Equation. 5.7 Discretization of the Low-Frequency Small-Disturbance Equation. A Solution of the diagonal system of equations A.1 Three diagonal Equation System A.2 Quad-Diagonal Matrix System B Selected Papers paperback, size 20,5 x 29 cm , English , 152 pages