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Özel Aralık Girişi
Comparison between blade element momentum theory and computational fluid dynamics methods for performance prediction of marine propellers
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 2017
KAYHAN ÜLGEN
Şakir Bal Tez Yüksek Lisans Tamamlandı
Nonlinear Correction to Blade Element Momentum Theory for Marine Propellers
International Symposium on Naval Architecture and Maritime (INT-NAM 2018), 24 Nisan 2018, s. 917-926
KARAALİOĞLU MEHMET SALİH,BAL ŞAKİR
Şakir Bal Tam metin bildiri
Investigation of Cavitating Marine Propeller Performance Using Blade Element Momentum Theory
3rd International Meeting - Progress in Propeller Cavitation and its Consequences:Experimental and Computational Methods for Predictions, İstanbul/TÜRKİYE, 15 Kasım 2018, s. 129-134
KARAALİOĞLU MEHMET SALİH,BAL ŞAKİR
Şakir Bal Tam metin bildiri
Nonlinear Large Angle Solution of Blade Element Momentum Theory for Marine Propellers
4th International Conference on Advances in Mechanical Engineering (ICAME 2018), İstanbul/TÜRKİYE, 19 Aralık 2018, s. 960-974
SOYDAN AHMET,BAL ŞAKİR
Şakir Bal Tam metin bildiri
Application of Classical Blade Element Momentum Theory and a Boundary Element Method to Cavitating Marine Current Turbines
1st International Symposium on Naval Architecture and Maritime (INT-NAM 2011), 24 Ekim 2011, s. 307-316
USAR D, BAL S
Şakir Bal Tam metin bildiri
Performance prediction of cavitating marine current turbine by BEMT based on CFD
OCEAN ENGINEERING, Vol. 255, Temmuz 2022, ISSN: 0029-8018
KARAALİOĞLU MEHMET SALİH, BAL ŞAKİR
Şakir Bal Özgün Makale Marine current turbineCavitationBlade element momentum theoryOpenFOAMPanel methodHYDRODYNAMIC PERFORMANCENUMERICAL-SIMULATIONCLOUD CAVITATIONTIDAL TURBINESDESIGNFLOWMODELTIPTECHNOLOGIESHYDROFOILS
Rotor Aerodynamics and Performance Enhancement via Active Trailing Edge Flaps
8th Asian / Australian Rotorcraft Forum, ANKARA/TÜRKİYE, 30 Ekim 2019, s. 1-7
URAL HÜSEYİN, ÖZDEMİR ÖZGE
Hüseyin Ural Tam metin bildiri Blade Element Momentum TheoryActive Trailing Edge FlapRotor Blade AerodynamicsHover
Rotor Aerodynamics and Performance Enhancement via Active Trailing Edge Flaps
8th Asian / Australian Rotorcraft Forum, ANKARA/TÜRKİYE, 30 Ekim 2019, s. 1-7
URAL HÜSEYİN, ÖZDEMİR ÖZGE
Özge Özdemir Tam metin bildiri Blade Element Momentum TheoryActive Trailing Edge FlapRotor Blade AerodynamicsHover

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