Yavuz Yaman

E-mail

yyaman@metu.edu.tr

Department

Department of Aerospace Engineering

ORCID

0000-0001-6278-059X

Scopus Author ID

6602735801

Web of Science Researcher ID

V-8861-2019

Uydularda Titreşim Test Sonuçları Kullanılarak Sonlu Elemanlar Modelinin Güncellenmesi Çekiç, Abdülkadir; Yaman, Yavuz (null; 2020-09-09)
Büyük Oranda Şekil Değiştiren İHA kanatlarının Modellenmesi, İncelenmesi ve Üretimi. ODTU den 2007'den itibaren katkılar Yaman, Yavuz (2020-01-01)
Seyir Füzesi Kanatlarındaki Aeroelastik Verimde Tasarım Girdilerinin Etkisi Yaman, Yavuz (2020-01-01)
Fatigue Test of a Structure Instrumented with Fibre Bragg Grating Sensors for Structural Health Monitoring Applications Karataş, Cansu; Değerliyurt, Boray; Şahin, Melin; Yaman, Yavuz (2019-10-30)
Generation of Helicopter Pull-Up Maneuver with Harmony Search Optimization Method Yaman, Yavuz; Kalkan, Uğur; Tıraş, Harun (null; 2019-10-30)
Passive Vibration Isolation of Jet Aircraft Avionics Equipment Yaman, Yavuz (null; 2019-09-20)
Effects of Various Design Parameters on the Performance of a Cruise Missile Wing Yaman, Yavuz (null; 2019-09-18) The design of a cruise missile wing is a multidisciplinary work because the wing has to provide enough aerodynamic forces while being structurally in safe. Various parameters of the wing are investigated during the design ...
Assessment of the Performance of a Cruise Missile Wing Depending on Design Parameters at Various Flight Conditions Ertürk, Burak; Yaman, Yavuz (2019-09-03) The design of a cruise missile wing is a multidisciplinary work, since the wing has to provide enough aerodynamic forces while being structurally safe. In order to meet the design requirements and achieve a successful desi...
Comparison of Performance of Surface Mounted and Embedded Fibre Bragg Grating Sensors under Fatigue Torsion Load Değerliyurt, Boray; Karataş, Cansu; Şahin, Melin; Yaman, Yavuz (null; 2019-05-21)
Synthesis, Analysis, and Design of a Novel Mechanism for the Trailing Edge of a Morphing Wing Şahin, Harun Levent; Yaman, Yavuz (MDPI AG, 2018-12-11) In the design and analysis of morphing wings, several sciences need to be integrated. This article tries to answer the question, “What is the most appropriate actuation mechanism to morph the wing profile?” by introducing ...

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