ARAMA SONUÇLARI

Toplam 24 adet sonuçtan 20 tanesi görüntülenmektedir.

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Özel Aralık Girişi

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
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
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
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
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
Supersonic coaxial flows Part 1 Free jets
9th (Millennium) International Symposium on Flow Visualisation, 22 Ağustos 2000
OZKAN GOKHAN,ÖZDEMİR İLYAS BEDİİ
Interactions of a supersonic jet and a perforated plate
9th (Millennium) International Symposium on Flow Visualisation, 22 Ağustos 2000
OZKAN GOKHAN,ÖZDEMİR İLYAS BEDİİ
Supersonic jet wall interactions
Eighth International Symposium on Flow Visualisation, 1 Eylül 1998
KAYISBUDAK METE,ÖZDEMİR İLYAS BEDİİ
Supersonic jet-wall interactions in model rocket launchers
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 1998
METİN UÇAK
İlyas Bedii Özdemir Tez Yüksek Lisans Tamamlandı
Numerical investigation of aerodynamic and aeroacoustic properties of a supersonic jet
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 2015
RAMİZ ÖMÜR İÇKE
İlyas Bedii Özdemir Tez Yüksek Lisans Tamamlandı
Shock characteristics of supersonic two phase free jets
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 2000
GÖKHAN ÖZKAN
İlyas Bedii Özdemir Tez Yüksek Lisans Tamamlandı
Implementation of propulsion system integration losses to a supersonic military aircraft conceptual design
Lisansüstü Eğitim Enstitüsü, İstanbul Teknik Üniversitesi, 2021
EMRE KARASELVİ
Melike Nikbay Tez Yüksek Lisans Tamamlandı
A high-order finite-volume solver for supersonic flows
Lisansüstü Eğitim Enstitüsü, İstanbul Teknik Üniversitesi, 2022
GREGORIO GERARDO SPINELLI
Bayram Çelik Tez Doktora Tamamlandı
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
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
Bayram Çelik Özgün Makale
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
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
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
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
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
Melike Nikbay Tam metin bildiri

İLETİŞİM BİLGİLERİ

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