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AIAA Aviation 2021 FORUM, 2 Ağustos 2021
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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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Investigation of Nacelle Design Parameters for a Supersonic Aircraft with Low Fidelity Approaches
11th Ankara International Aerospace Conference (AIAC), Ankara (Virtual)/TÜRKİYE, 8 Eylül 2021
OMER OZYILMAZ, NİKBAY MELİKE
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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
IMRAK RUMED, KARASELVİ EMRE, TUTKUN BÜLENT, 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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Reliability Based Design Optimization of a Supersonic Engine Inlet
2021 AIAA Propulsion and Energy Forum, Denver (Virtual)/AMERİKA BİRLEŞİK DEVLETLERİ, 9 Ağustos 2021
TEKASLAN HÜSEYİN EMRE, IMRAK RUMED, NİKBAY MELİKE
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Supersonic coaxial flows Part 1 Free jets
9th (Millennium) International Symposium on Flow Visualisation, 22 Ağustos 2000
OZKAN GOKHAN,ÖZDEMİR İLYAS BEDİİ
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Interactions of a supersonic jet and a perforated plate
9th (Millennium) International Symposium on Flow Visualisation, 22 Ağustos 2000
OZKAN GOKHAN,ÖZDEMİR İLYAS BEDİİ
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Supersonic jet wall interactions
Eighth International Symposium on Flow Visualisation, 1 Eylül 1998
KAYISBUDAK METE,ÖZDEMİR İLYAS BEDİİ
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Shock characteristics of supersonic two phase free jets
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 2000
GÖKHAN ÖZKAN
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Supersonic jet-wall interactions in model rocket launchers
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 1998
METİN UÇAK
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Numerical investigation of aerodynamic and aeroacoustic properties of a supersonic jet
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 2015
RAMİZ ÖMÜR İÇKE
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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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A high-order finite-volume solver for supersonic flows
Lisansüstü Eğitim Enstitüsü, İstanbul Teknik Üniversitesi, 2022
GREGORIO GERARDO SPINELLI
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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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A 2-D Finite Volume Navier-Stokes Solver for Supersonic Flows
Anadolu Üniversitesi Bilim ve Teknoloji Dergisi :A-Uygulamalı Bilimler ve Mühendislik, Vol. 18, No. 5, Aralık 2017, s. 1042-1056, ISSN: 1302-3160
TÜRK ADEM GÜRKAN,ÇELİK BAYRAM
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Multifidelity Sonic Boom Minimization of A Supersonic Aircraft
AIAA Scitech Forum, Tennessee (Virtual)/AMERİKA BİRLEŞİK DEVLETLERİ, 11 Ocak 2021
YUSUF DEMİROĞLU, YILDIZ ŞIHMEHMET, 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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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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