Taktik insansız hava araçlarının göreve uyumlu kanatlarında kambur ve burulma etkisinin çırpma ve kontrol yönünden analizi

2011-03-31
Şahin, Melih
Yaman, Yavuz
Özgen, Serkan
Seber, Güçlü

Suggestions

Taktik insansız hava aracı tasarımı ve üretimi
Oran, Can Mehmet; Başkan Perçin, Özge; Demircan, Alpay; Alemdaroğlu, Nafiz; Çiftçi, Meltem; Seber, Güçlü; Kayran, Altan; Özöztürk, Sedat; Demir, Özgür; Buzkıran, Mete(2012)
Proje kapsamında taktik bir insansız hava aracı tasarımı ve üretimi gerçekleştirilmiştir. Hava aracı bütünü ile kompozit malzemeden üretilmiştir. Hava aracı üretimi için gerekli olan bütün kalıplar da proje kapsamında Havacılık ve Uzay Mühendisliği Bölümü prototip atelyesinde üretilmiş ve proje sayesinde çok önemli bir üretim kabiliyeti sağlanmıştır. Hava aracının bütün mekanik ve elektromekanik sistem entegrasyonu başarı ile tamamlanmıştır. Hava aracına takılı bir kamera ve ver...
Reliability analysis of tactical unmanned aerial vehicle (UAV)
Koç, Yılmaz; Alemdaroğlu, Hüseyin Nafiz; Sürücü, Barış; Department of Aerospace Engineering (2017)
To design cost effective and reliable products are considered to be important to be competitive in the Aerospace Industry. Reliability is therefore, taken as an integral part of the design process. Reliability, which is a kind of design parameter that affects cost and system safety, shall be taken into account in early phases of design process due to difficulties facing during changes in design at the later phases. Reliability of Tactical UAVs can be evaluated by reliability testing but these tests are very...
Analysis, design and test of a jet vane based thrust vector control for tactical missiles
Eren, Oğuz; Eyi, Sinan; Department of Aerospace Engineering (2017)
In this thesis, a design effort for a jet vane based Thrust Vector Control (TVC) in the scope of mechanical design, computational analysis and validating test process is executed to be able to find an optimum CFD approach to this kind of work. To do that, a preliminary design phase is initiated with an already optimized geometry which provides an aerodynamic surface to be worked on. After mechanical design approach to the geometry with system requirements, some of the unverified aspects of the design are te...
Design and manufacturing of a tactical unmanned air vehicle
Şenelt, Engin; Alemdaroğlu, Hüseyin Nafiz; Department of Aerospace Engineering (2010)
The aim of this study is to describe the conceptual design, performance analysis to validate the design and manufacturing steps of Middle East Technical University Tactical Unmanned Air Vehicle (METU TUAV). The system requirements are adopted from a market study and assumed as is. Utilizing competitor search and conceptual design methodology, the rough parameters of the aircraft are defined and a performance analysis is conducted to validate the requirements. After the design team is content that the design...
Design of a medium range tactical UAV and improvement of its performance by using winglets
Turanoğuz, Eren; Alemdaroğlu, Hüseyin Nafiz; Department of Aerospace Engineering (2014)
The study encompasses the design, performance analysis and aerodynamic improvement of the designed medium range tactical unmanned aerial vehicle. Main requirements are set as following; cruising altitute above 3500m, endurance of approximately 10-12 hours, range of 150 km and payload of 60 kg. The conventional design phase is based on the employment of historical equations and experiences. Nowadays, employement of well known equations and experiences during the desing process are not enough to reveal a comp...
Citation Formats
M. Şahin, Y. Yaman, S. Özgen, and G. Seber, “Taktik insansız hava araçlarının göreve uyumlu kanatlarında kambur ve burulma etkisinin çırpma ve kontrol yönünden analizi,” 2011. Accessed: 00, 2022. [Online]. Available: https://hdl.handle.net/11511/95799.