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Toplam 34 adet sonuçtan 20 tanesi görüntülenmektedir.

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Özel Aralık Girişi

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
Numerical Investigation of Boundary Layer Bleed Effects on Supersonic Air Intake Performance
INTERNATIONAL GRADUATE RESEARCH SYMPOSIUM - IGRS'22, İstanbul/TÜRKİYE, 1 Haziran 2022
KOÇ OSMAN KEREM, YILDIZELİ ALPEREN, ÇADIRCI SERTAÇ, KOÇ İLKER MURAT
Multi-Fidelity Low-Rank Approximations for Uncertainty Quantification of a Supersonic Aircraft Design
MDPI Algorithms, Vol. 15, No. 7, Temmuz 2022, ISSN: 1999-4893
YILDIZ ŞIHMEHMET, PEHLİVAN SOLAK HAYRİYE, 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
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
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
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
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
Multi-Fidelity Low-Rank Approximations for Uncertainty Quantification of a Supersonic Aircraft Design
Algorithms, Temmuz 2022, ISSN: 1999-4893
YILDIZ ŞIHMEHMET, PEHLİVAN SOLAK HAYRİYE, NİKBAY MELİKE
Şıhmehmet Yıldız Özgün Makale
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
Şıhmehmet Yıldız Tam metin bildiri
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 coaxial flows Part 1 Free jets
9th (Millennium) International Symposium on Flow Visualisation, 22 Ağustos 2000
OZKAN GOKHAN,ÖZDEMİR İLYAS BEDİİ
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
Experimental investigation of underexpanded transverse jet interaction with supersonic crossflow
Lisansüstü Eğitim Enstitüsü, İstanbul Teknik Üniversitesi, 2022
UTKUN ERİNÇ MALKOÇOĞLU
Nuriye Leman Okşan Çetiner Yıldırım 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
Supersonic jet-wall interactions in model rocket launchers
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 1998
METİN UÇAK
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
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
Unsteady features of a supersonic jet approaching to a passage on a plate
23rd International Symposium on Shock Waves, 22 Temmuz 2001
OZKAN GOKHAN,DOLEK OMER,ÖZDEMİR İLYAS BEDİİ

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