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Özel Aralık Girişi

Sonic Boom Prediction Code Development and Sonic Boom Predictions via Open-Source CFD Software
Havacılık ve Uzay Teknolojileri Dergisi, Vol. 15, No. 2, Ocak 2022, ISSN: 1304-0448
ALPMAN EMRE, KAVURMACIOĞLU LEVENT ALİ, EKEN SEHER, İNCİ HARUN, ÇAMUR ZELİHA, BİÇER BARIŞ
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
Implementation of Multidisciplinary and Multifidelity Uncertainty Quantification Methods for Sonic Boom Prediction
American Institute of Aeronautics and Astronautics (AIAA), Ocak 2022, ISSN: 0021-8669
TEKASLAN HÜSEYİN EMRE, YILDIZ ŞIHMEHMET, DEMİROGLU YUSUF, NİKBAY MELİKE
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
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
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
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
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
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
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
Melike Nikbay Özgün Makale sonic boom
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
Implementation of Multidisciplinary and Multifidelity Uncertainty Quantification Methods for Sonic Boom Prediction
Journal of Aircraft, Aralık 2022, ISSN: 1533-3868
TEKASLAN HÜSEYİN EMRE, YILDIZ ŞIHMEHMET, DEMİROĞLU YUSUF, NİKBAY MELİKE
Şıhmehmet Yıldız Özgün Makale
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
Şıhmehmet Yıldız Tam metin bildiri
Sizing and prestress optimization of Class-2 tensegrity structures for space boom applications
ENGINEERING WITH COMPUTERS, Vol. 38, No. 2, Ocak 2022, ISSN: 0177-0667
YILDIZ KAAN, LESİEUTRE GEORGE A
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
A New Method to Assess the Machine Design Parameters on the Stability of Boom Tunnelling Machine
20th World Mining Congress, 7 Kasım 2005, s. 691-698
ESKIKAYA S,ACAROĞLU ERGÜN ÖMÜR,ERGIN H
Ömür Acaroğlu Ergün Tam metin bildiri
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
Melike Nikbay Bilimsel Kitap
Production of a Helicopter Tail Boom and Associated Mechanical Tests
Advanced Materials Research, Vol. 445, Ocak 2012, s. 566-570, ISSN: 1662-8985
TÜRKMEN HALİT SÜLEYMAN,DENİZ KAVRAR,M LUTFY ÖVEÇOĞLU
Halit Süleyman Türkmen Özgün Makale
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
Vedat Ziya Doğan Özgün Makale

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