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Преглед према Аутор Petrović, Milan

Приказ резултата 1 до 20 од 95  следеће >
ГодинаНасловАутор(и)Тип резултатаМп-кат.
2021A Comprehensive Analytical Shock Loss Model for Axial Compressor CascadesBanjac, Milan  ; Savanović, Teodora  ; Petković, Đorđe  ; Petrović, Milan  Conference Paper
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2022A Comprehensive Analytical Shock Loss Model for Axial Compressor CascadesBanjac, Milan  ; Savanović, Teodora  ; Petković, Đorđe  ; Petrović, Milan  Научни чланак
22M22 - Међународни часопис категорије M22
2014A New Loss and Deviation Model for Axial Compressor Inlet Guide VanesBanjac, Milan  ; Petrović, Milan  ; Wiedermann, AlexanderArticle
22M22
2015A Quick Method for Full Flange-to-flange Industrial Gas Turbine Analysis Based on Through-flow ModellingPetrović, Milan  ; Alexander Wiedermann; Ahmed Abdel-RahmanConference Paper
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2016A quick method for full flange-to-flange industrial gas turbine analysis based on through-flow modellingPetrović, Milan  ; Alexander Wiedermann; Ahmed Abdel-RahmanArticle
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2016A simple model for thermodynamic properties of air and combustion gases for educational purposesBanjac, Milan  ; Milić, Srđan  ; Petrović, Milan  Конференцијски рад
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2013Aerodynamic Calculation of Siemens Gas Turbines SGT-4000FPetrović, Milan  Technical reports
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2014Aerodynamic Design Of Air-Cooled Gas TurbinesPetrović, Milan  Conference Paper
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2012Analiza rada kondenzatorskog dela parnog turbopostrojenja bloka A6Petrović, Milan  ; Miloš DespićТехничко решење
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2016Analiza rada kondenzatorskog postrojenja u TE Morava 120 MWMilić, Srđan  ; Banjac, Milan  ; Nedeljković, Srećko  ; Ranković, Miloš ; Đukanović, Dejan  ; Petrović, Milan  ; Marija Stevanovic; Gordana NovakovićConference Paper
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2018Analysis of operation of the condenser in a 120 mw thermal power plantMilić, Srđan  ; Petrović, Milan  ; Banjac, Milan  ; Đukanović, Dejan  ; Nedeljković, Srećko  Article
22M22
2023Axial Compressor Design System with Direct Generation of 3D GeometryBanjac, Milan  ; Petković, Đorđe  ; Madžar, Teodora; Petrović, Milan  Conference Paper
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2012Calculation of Flow and Overall Performances of SGT5-8000H NG50 Siemens Gas TurbinePetrović, Milan  Техничко решење
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2013Calculation of Flow and Overall Performances of SGT5-8000H NG60 Siemens Gas Turbine -NG60 1.3 at upper limit load and ambient pressure 900 mbar/920 mbar/950 mbar/980 mbar /1013 mbar /1020 mbar /1030 mbar/1045 mbarPetrović, Milan  Техничко решење
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2013Calculation of Flow and Overall Performances of SGT5-8000H NG60 Siemens Gas Turbine -NG60 1.4 at upper limit load and ambient pressure 900 mbar / 920 mbar / 950 mbar / 980 mbar / 1013 mbarPetrović, Milan  Technical reports
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2012Calculation of the SGT6-8000H NG60-Siemens Gas Turbine Flow varying boundary conditions and radial tip gapsPetrović, Milan  Technical reports
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2025Comprehensive Method for Predicting Gas Turbine Cycle Performances Considering the Impact of Various FuelsPetrović, Milan  ; Petković, Đorđe  ; Milić, Srđan  ; Wiedermann, Alexander; Krewinkel, RobertConference Paper
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2025Comprehensive Method For Predicting Gas Turbine Cycle Performances Considering The Impact Of Various FuelsPetrović, Milan  ; Petković, Đorđe  ; Milić, Srđan  ; Wiedermann, Alexander; Krewinkel, RobertНаучни чланак
22M22 - Међународни часопис категорије M22
2010Development and validation of a new universal through flow method for axial compressorsPetrović, Milan  ; Wiedermann, A; Banjac, Milan  Article
22M22
2009Development and validation of a new universal through flow method for axial compressorsPetrović, Milan  ; Wiedermann, Alexander; Banjac, Milan  Conference Paper
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