Implementation of Multidisciplinary and Multifidelity Uncertainty Quantification Methods for Sonic Boom Prediction
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Sonic Boom Prediction Code Development and Sonic Boom Predictions via Open-Source CFD Software
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ALPMAN EMRE, KAVURMACIOĞLU LEVENT ALİ, EKEN SEHER, İNCİ HARUN, ÇAMUR ZELİHA, BİÇER BARIŞ
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Shape Optimization Methodology for Reducing the Sonic Boom Initial Pressure Rise
American Institute of Aeronautics and Astronautics (AIAA), Vol. 45, No. 5, Mayıs 2007, s. 1007-1018, ISSN: 0001-1452
FARHAT CHARBEL, MAUTE KURT, ARGROW BRİAN, 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
YUSUF DEMİROĞLU, 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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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 Methodology for Reducing the Sonic Boom Initial Pressure Rise
AIAA Journal, Vol. 45, No. 5, 2007, s. 1007-1018
CHARBEL FARHAT,KURT MAUTE,BRİAN ARGROW,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
DEMİROĞLU YUSUF, YILDIZ ŞIHMEHMET, 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
TEKASLAN HÜSEYİN EMRE, YILDIZ ŞIHMEHMET, DEMİROĞLU YUSUF, NİKBAY MELİKE
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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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Development of a nonlinear sonic boom propagation code
Lisansüstü Eğitim Enstitüsü, İstanbul Teknik Üniversitesi, 2023
YUSUF DEMİROĞLU
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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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Coupled Sensitivity Analysis by Discrete-Analytical Direct and Adjoint Methods with Applications to Aeroelastic Optimization and Sonic Boom Minimization”
Boulder/AMERİKA BİRLEŞİK DEVLETLERİ, 2002, University of Colorado at Boulder
NİKBAY MELİKE
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Multifidelity Sonic Boom Minimization of A Supersonic Aircraft by Parametric Wing Shape Design
AIAA Scitech Forum, Tennessee (Virtual)/AMERİKA BİRLEŞİK DEVLETLERİ, 11 Ocak 2021
YUSUF DEMİROĞLU, YILDIZ ŞIHMEHMET, NİKBAY MELİKE
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Dynamic Multimode Response of Composite Plates to Sonic Boom and Blast Loadings
Journal of Aircraft, Vol. 45, No. 2, Mart 2008, s. 498-507, ISSN: 0021-8669
DOĞAN VEDAT ZİYA
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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
YILDIZ ŞIHMEHMET, DEMİROGLU YUSUF, NİKBAY MELİKE
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Impact of Aeroelastic Uncertainties on Sonic Boom Signature of a Commercial Supersonic Transport Configuration
AIAA Scitech Forum, Dallas/AMERİKA BİRLEŞİK DEVLETLERİ, 9 Ocak 2017
NİKBAY MELİKE,STANFORD BRET,WEST TOM,RALLABHANDİ SRİRAM
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