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İSTANBUL TEKNİK ÜNİVERSİTESİ UÇAK VE UZAY BİLİMLERİ FAKÜLTESİ UZAY MÜHENDİSLİĞİ BÖLÜMÜ

Ana Dal Mühendislik Temel Alanı
Yan Dal Uçak-Havacılık-Uzay Mühendisliği

Kayıtlı çıktılara kısa bakış — ayrıntılar aşağıda.

Makale 28
Proje 0
Kitap 13
Bildiri 73
Patent 0
Sanatsal 0

Scopus (SJR) Q1 8 Q2 8 Q3 1 Q4 0

WoS (JCR) Q1 3 Q2 9 Q3 6 Q4 1

TR Index 0 makale

Alan+yıl+tür normalize OpenAlex yüzdelik — Clarivate ESI / SciVal değildir.

Üst %1 makale 0

Üst %10 makale 4

Ort. yüzdelik 69.2%

Üst %1 payı 0.0%

Üst %10 payı 22.2%

Makaleler

YÖKSİS ve OpenAlex kaynak ayrımıyla makaleler; quartile ve TR Index ile daraltabilirsiniz.

Makale listesi

2025 Aeroacoustic optimization of unsteady transonic cavity flow using a Bayesian approach CEAS Aeronautical Journal DOI 10.1007/s13272-025-00866-7 YÖKSİS SJR Q2 JCR Q2 OpenAlex 16.8%
2025 Analytical benchmark problems and methodological framework for the assessment and comparison of multifidelity optimization methods. Archives of Computational Methods in Engineering DOI 10.1007/s11831-025-10392-8 YÖKSİS SJR Q1 JCR Q1 OpenAlex 85.4%
2024 Low Observable Uncrewed Aerial Vehicle Wind Tunnel Model Design, Manufacturing, and Aerodynamic Characterization Aerospace DOI 10.3390/aerospace11030216 YÖKSİS SJR Q2 JCR Q2 OpenAlex üst %10 OpenAlex 94.3%
2023 Numerical Investigations on Low-Speed Aerodynamic Characteristics of Generic Unmanned Combat Aerial Vehicle Configurations American Institute of Aeronautics and Astronautics (AIAA) Journal of Aircraft DOI 10.2514/1.C037258 YÖKSİS SJR Q1 JCR Q2 OpenAlex 56.4%
2023 Conceptual Design of a Nonconstant Swept Flying Wing Unmanned Combat Aerial Vehicle American Institute of Aeronautics and Astronautics (AIAA) Journal of Aircraft DOI 10.2514/1.C037257 YÖKSİS SJR Q1 JCR Q2 OpenAlex 84.0%
2023 Multifidelity Prediction Framework with Convolutional Neural Networks Using High-Dimensional Data American Institute of Aeronautics and Astronautics (AIAA) Journal of Aerospace Information Systems DOI 10.2514/1.I011159 YÖKSİS JCR Q2 OpenAlex 67.6%
2023 Implementation of Multidisciplinary and Multifidelity Uncertainty Quantification Methods for Sonic Boom Prediction American Institute of Aeronautics and Astronautics (AIAA) Journal of Aircraft DOI 10.2514/1.C036962 YÖKSİS SJR Q1 JCR Q2 OpenAlex 79.0%
2022 Editorial: Uncertainty quantification in characterization, modelling, and design of materials Frontiers in Materials DOI 10.3389/fmats.2022.1111499 YÖKSİS SJR Q2 JCR Q3
2022 Multi-Fidelity Low-Rank Approximations for Uncertainty Quantification of a Supersonic Aircraft Design MDPI Algorithms DOI 10.3390/a15070250 YÖKSİS SJR Q2 JCR Q2 OpenAlex 65.5%
2019 Internal Ballistic Modeling of a Solid Rocket Motor by Analytical Burnback Analysis Journal of Spacecraft and Rockets DOI 10.2514/1.A34065 YÖKSİS SJR Q1 JCR Q3 OpenAlex üst %10 OpenAlex 97.3%
2018 Solid rocket motor design using a surrogate model AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY DOI 10.1108/AEAT-01-2017-0045 YÖKSİS SJR Q2 JCR Q3 OpenAlex 43.9%
2018 Solid Rocket Motor Propellant Optimization with Coupled Internal Ballistic–Structural Interaction Approach Journal of Spacecraft and Rockets DOI 10.2514/1.A34066 YÖKSİS SJR Q2 JCR Q3 OpenAlex üst %10 OpenAlex 97.8%
2015 Development of a nanosatellite de orbiting system by reliability based design optimization Acta Astronautica DOI 10.1016/j.actaastro.2015.09.002 YÖKSİS SJR Q1 JCR Q1 OpenAlex 18.0%
2010 Reliability based aeroelastic optimization of a composite aircraft wing via fluid structure interaction of high fidelity solvers IOP Conference Series: Materials Science and Engineering DOI 10.1088/1757-899X/10/1/012037 YÖKSİS OpenAlex 82.2%
2009 Multidisciplinary Code Coupling for Analysis and Optimization of Aeroelastic Systems AIAA Journal of Aircraft DOI DOI:10.2514/1.41491 YÖKSİS OpenAlex üst %10 OpenAlex 92.8%
2008 Sonic boom mitigation via shape optimization using an adjoint method and application to a supersonic fighter aircraft European Journal of Computational Mechanics DOI 10.3166/remn.17.217-243 YÖKSİS JCR Q3 OpenAlex 77.9%
2007 Shape Optimization Methodology for Reducing the Sonic Boom Initial Pressure Rise American Institute of Aeronautics and Astronautics (AIAA) DOI 10.2514/1.27607 YÖKSİS SJR Q1 JCR Q1 OpenAlex 87.9%
2025 Aeroacoustic Optimization of Unsteady Transonic Cavity Flow using a Bayesian Approach CEAS Aeronautical Journal DOI 10.1007/s13272-025-00866-7 YÖKSİS SJR Q2 JCR Q2 OpenAlex 16.8%
2016 Aeroelastic Predictions for Steady and Unsteady Flow Characteristics of HIRENASD Wing Progress in Computational Fluid Dynamics DOI http://www.inderscience.com/jhome.php?jcode=pcfd YÖKSİS SJR Q3 JCR Q4
2015 Reduced Order Modelling of Static and Dynamic Aeroelastic Predictions withMultidisciplinary Approach CEAS Aeronautical Journal / Springer DOI DOI10.1007/s13272-015-0154-3 YÖKSİS SJR Q2 JCR Q2

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