The papers present an analysis of the advantages and disadvantages of application joined wing layout for unmanned aerial vehicle. Synthesis of optimal layout by criteria for aerodynamic efficiency, flight duration and weight of the structure are given in the article
Possibility of application joined wing layout for UAV
01.10.2015
2186670 byte
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Hybrid wing body-joined wing layout hydrogen energy aircraft adopting injection type power fan
Europäisches Patentamt | 2024
|Multi-disciplinary coupling optimization design method for integrated joined wing layout
Europäisches Patentamt | 2025
|NTIS | 2008
|Joined-Wing Configuration Aerodynamics
British Library Online Contents | 1996
|