Investigation and Improvement of Supersonic Intake Flow Characteristics Using Boundary Layer Control Techniques
Lisansüstü Eğitim Enstitüsü, İstanbul Teknik Üniversitesi, 2023
FERHAT ÇETİN
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Investigation of Shock-Vortex Interactions in Supersonic Flows via a High-Order Finite Volume Solver
Lisansüstü Eğitim Enstitüsü, İstanbul Teknik Üniversitesi, 2023
LADİN NİL KOFOĞLU
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Investigation of Shock-Vortex Interactions in Supersonic Flows via a High-Order Finite Volume Solver
Lisansüstü Eğitim Enstitüsü, İstanbul Teknik Üniversitesi, 2023
LADİN NİL KOFOĞLU
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Surrogate-based design optimization for a supersonic diverterless intake
Fen Bilimleri Enstitüsü, Orta Doğu Teknik Üniversitesi, 2024
SANEM ÇALIŞ GEBOLOĞLU
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A high-order finite-volume solver for supersonic flows
Lisansüstü Eğitim Enstitüsü, İstanbul Teknik Üniversitesi, 2022
GREGORIO GERARDO SPINELLI
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Experimental investigation of underexpanded transverse jet interaction with supersonic crossflow
Lisansüstü Eğitim Enstitüsü, İstanbul Teknik Üniversitesi, 2022
UTKUN ERİNÇ MALKOÇOĞLU
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Implementation of propulsion system integration losses to a supersonic military aircraft conceptual design
Lisansüstü Eğitim Enstitüsü, İstanbul Teknik Üniversitesi, 2021
EMRE KARASELVİ
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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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Multidisciplinary Uncertainty Quantification in Aeroelastic Analyses of Semi Span Supersonic Transport Wing
AIAA Aviation and Aeronautics Forum and Exposition, 22 Haziran 2015
NİKBAY MELİKE,PİNAR ACAR
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APPLICATIONS OF ADAPTIVE MESH REFINEMENT ON HIGH ORDER SOLVER FOR SUPERSONIC FLOWS
ParCFD’2020, 32nd International Conference on Parallel Computational Fluid Dynamics, Nice/FRANSA, 11 Mayıs 2021
SPİNELLİ GREGORİO GERARDO, ÇELİK BAYRAM
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Numerical Investigation of Boundary Layer Bleed Effects on Supersonic Air Intake Performance
INTERNATIONAL GRADUATE RESEARCH SYMPOSIUM – IGRS’22, istanbul/TÜRKİYE, 1 Haziran 2022
KOÇ OSMAN KEREM,YILDIZELİ ALPEREN,ÇADIRCI SERTAÇ,KOÇ İLKER MURAT
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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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Multi-Fidelity and Multi-Disciplinary Design Optimization of A Low-Boom Supersonic Transport Aircraft
2023 AIAA Scitech Forum, National Harbor, Maryland/AMERİKA BİRLEŞİK DEVLETLERİ, 23 Ocak 2023
NİKBAY MELİKE, KILIÇ DİLAN, ÇAKMAK ENES, TEKASLAN HÜSEYİN EMRE, YILDIZ ŞIHMEHMET, DEMİROGLU YUSUF
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Multi-Fidelity and Multi-Disciplinary Design Optimization of A Low-Boom Supersonic Transport Aircraft
AIAA Scitech 2023, 23 Ocak 2023
NİKBAY MELİKE, KILIÇ DİLAN, ÇAKMAK ENES, TEKASLAN HÜSEYİN EMRE, YILDIZ ŞIHMEHMET, DEMİROĞLU YUSUF
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Numerical Investigation of Boundary Layer Bleed Effects on Supersonic Air Intake Performance
International Graduate Research Symposium – IGRS’22, 1 Haziran 2022
KOÇ OSMAN KEREM, YILDIZELİ ALPEREN, ÇADIRCI SERTAÇ, KOÇ İLKER MURAT
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A Multifidelity Steady and Unsteady Aerodynamic Prediction Framework with Deep Neural Networks
2022 AIAA Aviation Forum, Chicago/AMERİKA BİRLEŞİK DEVLETLERİ, 27 Haziran 2022
TEKASLAN HÜSEYİN EMRE, NİKBAY MELİKE
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Surrogate Unsteady Aerodynamic Modeling with Autoencoders and Long-Short Term Memory Networks
2022 AIAA Scitech Forum, San Diego (Online)/AMERİKA BİRLEŞİK DEVLETLERİ, 3 Ocak 2022
TEKASLAN HÜSEYİN EMRE, DEMİROGLU YUSUF, NİKBAY MELİKE
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Implementation of Propulsion System Integration Losses to a Supersonic Military Aircraft Conceptual Design
AIAA Propulsion and Energy 2021 Forum, Virtual/AMERİKA BİRLEŞİK DEVLETLERİ, 9 Ağustos 2021
KARASELVİ EMRE, 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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