Beograd,1970. A4, meki povez, 158 strana u odličnom stanju

Beograd 1965. meki povez, 273 strane u dobrom stanju

Projektovanje, proizvodnja i eksploatacija autobusa by Stanislav Glumac, Srećko Žeželj, Pavle Gladović, Srećko Nijemčević TVRD POVEZ, 2002,IKARBUS Beograd,435.stranailustr. TEHNIČKA KNJIGA Knjiga je NOVA ----------------------------⭐️ M

Beograd 2013, mek povez, očuvanost 5/5- , 24 cm, 608 + 377 + 479 strana, težina oko 2,3 kg

➡️ http://www.kupindo.com/Clan/Chuma/SpisakPredmeta JAT - pilotska značka Dimenzije 7,2cm x 4,6cm Trenutno stanje vidite na slikama.

Made in Yugoslavia BAŠ RETKO Sve slikam neposredno pred postavljanje pa stanje bukvalno odgovara fotografijama. . Nakon dogovora uplata je na račun u OTP Banci Šaljem postexpresom nakon uplate Šaljem u inostranstvo jedino EMSOM (postexpres za inostranstvo pri pošti Srbije, skuplji je od klasičnog slanja ali sigurniji, i brži), gde vi snosite sve troškove slanja, za carinske troškove kupovine više predmeta ili gubitke paketa nisam odgovoran, , osim ako nemate nekoga u srbiji da pošaljem na njegovu adresu, nakon uplate na moj račun ili vaše uplate Western unionom na ime i podatke!

Četiri različite značke: - Titova štafeta 1950, 300 dinara - S Titom u ratu - s Titom u miru, 1945, Me-Ba, Zagreb, 2000 dinara - Za domovinu s Titom - napred, 1962, 800 dinara - Petokraka i NO, 400 dinara Može pojedinačna prodaja M O 4 K 3

Značka `Alfa Romeo` (na papučicu) u originalnoj kesici.Prečnik značke (bez papučice) 1,2cm. Vrlo dobro očuvana značka za svoje godine.Verovatno nikada nije boravila u albumu/panou.

CARTE DE PILOTAGE DU DANUBE, (LES BRAS BALA ET BORCEA) Echelle: 1:25 000 Na RUSKOM I FANCUSKOM I RUMUNSKOM jeziku. PLOVNE KARTE DUNAVA. Na prvih 18 strana knjige date su tablice sa oznakama i objašnjenjima upotrebe karata, kao i preporučena brzina plovidbe po označenim deonicama.+ 23.karte. DD

prečnik 26mm

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)

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 180 W (2x90 W) Frekventni opseg 50-20000 Hz Osetljivost 87 dB Impedansa 4 Ohm Niskotonac 130 mm PEI membrana Srednjotonac 30 mm "mylar" kalotni Visokotonac 15 mm piezo Vešanje Gumeno Materijal kucišta Aluminijum Velicina zvucnika 130 mm Ugradne dimenzije 122 mm (širina) x 52 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 180 W (2x90 W) Frekventni opseg 50-20000 Hz Osetljivost 87 dB Impedansa 4 Ohm Niskotonac 130 mm PEI membrana Srednjotonac 30 mm "mylar" kalotni Visokotonac 15 mm piezo Vešanje Gumeno Materijal kucišta Aluminijum Velicina zvucnika 130 mm Ugradne dimenzije 122 mm (širina) x 52 mm (dubina)

Karakteristike: Zvučnici za kola - 10cm Model: TS-G1010 Maksimalna izlazna snaga: 190 Watt Nominalna izlazna snaga: 30Watt Impedansa: 4? Raspon Frekvencije: 38 - 26,000 Hz Najniža rezonantna frekvencija: 124 Hz Osetljivost: 89 dB Veličina zvučnika: 10cm Materijal: IMPP kompozitna membrana Ugradna širina: 106 mm Ugradna dubina: 43 mm Karakteristike: Zvučnici za kola - 10cm Model: TS-G1010 Maksimalna izlazna snaga: 190 Watt Nominalna izlazna snaga: 30Watt Impedansa: 4? Raspon Frekvencije: 38 - 26,000 Hz Najniža rezonantna frekvencija: 124 Hz Osetljivost: 89 dB Veličina zvučnika: 10cm Materijal: IMPP kompozitna membrana Ugradna širina: 106 mm Ugradna dubina: 43 mm

Krug na cetiri coska - Bogdan Bogdanovic Krug na četiri ćoška: Demonijacka rasprava o okultnom poreklu pitagorejskih utopija propracena ponocnim razgovorima dvojice pitagorejskih disidenata sa pridodatim epilogom i iscrpnim bibliografskim komentarom i dovoljnim brojem dijagrama i nacrta odlicno stanje kospol

Najlepse gradjevine i prostori sveta - komplet 1-12 Tvrdi povezi sa omotnicama; Beograd, 1986/87. jako lepo / odlicno ocuvane knjige. - Hramovi moci - Domovi kraljeva - Sjaj bogova - Raskos religija - Arhitektura, covek, podneblje - Izazov prirodi - Gradjevine iz sna neimara - Svetista misticizma - Novi spomenici - U cast demokratije - Svet zadovoljstva - Pod okriljem vere

Naslov: Srednjevekovni gradovi u Srbiji, Crnoj Gori i Makedoniji Autor: Aleksandar Deroko Izdavač: Beograd : Prosveta Godina izdanja: 1950, 214 str., [1] presavijeni list s geogr. kartom : ilustr. ; 33 cm Povez: Tvrd Ćirilica Stanje 4 pokoji bibliotečki pečat S6 Pogledajte ostale knjige,časopise i stripove u ponudi http://www.kupindo.com/Clan/bdenis/SpisakPredmeta http://www.limundo.com/Clan/bdenis/SpisakAukcija

77 znacaka: vojne škole, oznake jedinica, divizije i brigade.

23x16mm

Udruženje emajliraca Jugoslavije, Zagreb, 1980.god. tvrd povez, 376 strana, knjiga ima potpis bivšeg vlasnika i dobro je očuvna

PANČEVAČKO SRPSKO CRKVENO PRAVOSLAVNO DRUŠTVO 1862 [K-21] Stanje : kao na slikama

KAMIONI I KOMBI VOZILA AUTOR: DRAGIŠA SIMONOVIĆ IZDAVAČ: TEHNIČKA KNJIGA, BEOGRAD GODINA IZDANJA: 1988. MEKE KORICE PISMO: LATINICA BROJ STRANA: 164 STR. STANJE KNJIGE VRLO DOBRO TROŠKOVE SLANJA SNOSI KUPAC LIČNO PREUZIMANJE MOGUĆE U CENTRU BEOGRADA STST NVK

Zbirka od oko 240 značaka. Značke su u albumu. Ima i rasparnih i serija... Pogledajte slike.

dobro stanje , 24 x 18 , 630 strana

58987) Computational Fluid Dynamics and Reacting Gas Flows , B. Engquist ; M. Luskin ; A. Majda ; editors ; Springer Verlag New York / Berlin 1988 , IMA Institute for Mathematics and Its Applications volume 12 ; This IMA Volume in Mathematics and its Applications COMPUTATIONAL FLUID DYNAMICS AND REACTING GAS FLOWS is in part the proceedings of a workshop which was an integral part of the 1986-87 IMA program on SCIENTIFIC COMPUTATION. We are grateful to the Scientific Committee: Bjorn Engquist (Chairman), Roland Glowinski, Mitchell Luskin and Andrew Majda for planning and implementing an exciting and stimulating year-long program. We especially thank the Workshop Organizers, Bjorn Engquist, Mitchell Luskin and Andrew Majda, for organizing a workshop which brought together many of the leading researchers in the area of computational fluid dynamics. George R. Sell Hans Weinberger PREFACE Computational fluid dynamics has always been of central importance in scientific computing. It is also a field which clearly displays the essential theme of interaction between mathematics, physics, and computer science. Therefore, it was natural for the first workshop of the 1986- 87 program on scientific computing at the Institute for Mathematics and Its Applications to concentrate on computational fluid dynamics. In the workshop, more traditional fields were mixed with fields of emerging importance such as reacting gas flows and non-Newtonian flows. The workshop was marked by a high level of interaction and discussion among researchers representing varied `schools of thought` and countries. hard cover, size 16 x 24 cm , ex library copy , 346 pages

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