Sonic Boom Prediction Code Development and Sonic Boom Predictions via Open-Source CFD Software
Havacılık ve Uzay Teknolojileri Dergisi, Vol. 15, No. 2, Ocak 2022, ISSN: 1304-0448
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Shape Optimization Methodology for Reducing the Sonic Boom Initial Pressure Rise
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Exploration of Optimal Propulsion System Airframe Integration Design Concepts for a Low Boom Supersonic Aircraft
AIAA Aviation Forum and Exposition, Washington, Washington (Virtual)/AMERİKA BİRLEŞİK DEVLETLERİ, 2 Ağustos 2021
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Shape Optimization Methodology for Reducing the Sonic Boom Initial Pressure Rise
AIAA Journal, Vol. 45, No. 5, 2007, s. 1007-1018
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Exploration of Optimal Propulsion System Airframe Integration Design Concepts for a Low Boom Supersonic Aircraft
AIAA Aviation 2021 FORUM, 2 Ağustos 2021
IMRAK RUMED, KARASELVİ EMRE, TUTKUN BÜLENT, NİKBAY MELİKE
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Sonic boom mitigation via shape optimization using an adjoint method and application to a supersonic fighter aircraft
European Journal of Computational Mechanics, Vol. 17, No. 1, Ocak 2008, s. 217-243, ISSN: 1779-7179
MAUTE KURT, FARHAT CHARBEL, ARGROW BRİAN, NİKBAY MELİKE
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A Comparative Study on Multi-Fidelity Sonic Boom Prediction for a Supersonic Aircraft
AeroBest 2021, An Eccomas Thematic Conference on Multidisciplinary Design Optimization of Aerospace Systems, Lisbon (Virtual)/PORTEKİZ, 21 Temmuz 2021
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Implementation of Multidisciplinary and Multifidelity Uncertainty Quantification Methods for Sonic Boom Prediction
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TEKASLAN HÜSEYİN EMRE, YILDIZ ŞIHMEHMET, DEMİROGLU YUSUF, NİKBAY MELİKE
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Implementation of Multidisciplinary Multi- Fidelity Uncertainty Quantification Methods in Sonic Boom Prediction
AIAA Aviation Forum and Exposition, Virtual/AMERİKA BİRLEŞİK DEVLETLERİ, 2 Ağustos 2021
TEKASLAN HÜSEYİN EMRE, YILDIZ ŞIHMEHMET, DEMİROGLU YUSUF, NİKBAY MELİKE
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Development of A Sonic Boom Propagation Code For Low-Boom Supersonic Aircraft Design and Optimization
AIAA SCITECH 2023 Forum, National Harbor, Maryland/AMERİKA BİRLEŞİK DEVLETLERİ, 23 Ocak 2023
DEMİROGLU YUSUF, NİKBAY MELİKE
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F Function Lobe Balancing for Sonic Boom Minimization
Computational Fluid Dynamics Journal, Vol. 17, No. 4, 2009, s. 221-234
BRİAN ARGROW,KURT MAUTE,CHARBEL FARHAT,NİKBAY MELİKE
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Shape Optimization with F Function Balancing for Reducing the Sonic Boom Initial Shock Pressure Rise
The International Journal of Aeroacoustics, Vol. 3, No. 4, 2004, s. 361-378
CHARBEL FARHAT,BRİAN ARGROW,NİKBAY MELİKE,KURT MAUTE
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Multi-fidelity Sonic Boom Minimization of a Supersonic Aircraft by Parametric Wing Shape Design
AIAA Scitech 2021 Forum, 11 Ocak 2021
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Implementation of Multidisciplinary and Multifidelity Uncertainty Quantification Methods for Sonic Boom Prediction
Journal of Aircraft, Mart 2023, ISSN: 1533-3868
TEKASLAN HÜSEYİN EMRE, YILDIZ ŞIHMEHMET, DEMİROĞLU YUSUF, NİKBAY MELİKE
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Implementation of Multidisciplinary Multi-Fidelity Uncertainty Quantification Methods in Sonic Boom Prediction
AIAA AVIATION 2021 FORUM, 6 Ağustos 2021
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Propulsion-Airframe Integration for Low-boom Supersonic Aircraft
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 2023
RUMED İMRAK
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Development of a nonlinear sonic boom propagation code
Lisansüstü Eğitim Enstitüsü, İstanbul Teknik Üniversitesi, 2023
YUSUF DEMİROĞLU
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Propulsion-airframe integration for low-boom supersonic aircraft
Lisansüstü Eğitim Enstitüsü, İstanbul Teknik Üniversitesi, 2023
RUMED İMRAK
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COMPARISON OF ANALYTICAL AND FINITE ELEMENT ANALYSISOF A TOWER CRANE BOOM
21st International Research/Expert Conference”Trends in the Development of Machinery and Associated Technology”TMT 2018, Karlovy Vary/ÇEK CUMHURİYETİ, 18 Eylül 2018
ŞAHİN UMUT,CANDAŞ ADEM,BOĞOÇLU MUHARREM ERDEM
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Ses-Ustu Bir Ucak Modelinin Govdesi icin Sonik Patlama Op- timizasyonu (Sonic Boom Minimization of a Supersonic Aircraft Fuselage)
8. Ulusal Havacilik ve Uzay Konferansi, Ankara/TÜRKİYE, 9 Eylül 2020
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