2 articles published in Asrel Aerospace Research Letters with the keyword "UAV": Design and Longitudinal Stability Analysis of a Stealth Unmanned Aerial Vehicle; Thermodynamic Analysis Of An Air Compressor Of Micro Turbojet Engines Used For Propulsion In UAVs
Zekiye Çinar, RABİA UZUN, Tolunay DAĞ, Tuğrul Oktay
Asrel Aerospace Research Letters, 2025, Vol 4, Issue 2, Page 153-167
This study includes the design and investigation stability of aircraft. The designed unnamed air vehicle (UAV) mission is conducting observation and gather intelligence without being detected by enemy radars. The designed UAV has fixed wing, mass of 10 kg and cruising speed of 30 m/s. The most...
Ali Ismayilli, Mahmut Sami Büker
Asrel Aerospace Research Letters, 2024, Vol 3, Issue 1, Page 27-43
In this study, computational fluid dynamics (CFD) and thermodynamic analyses of the radial compressor whell, one of the key components of the small-scale micro turbojet engine used for propulsion in UAV’s, were conducted. The micro turbojet engine was analyzed under sea level conditions (101.325...
İHASabit KanatGizlilik TeknolojisiBoylamasına KararlılıkFixed Wing Stealth TechnologyLongitudinal StabilityHava KompresörüTermodinamik AnalizMikro Turbojet MotoruMicro Turbojet EnginesAir CompressorThermodynamic Analysis
