Add to ORKGThe paper discusses the aerodynamic design improvement of a ducted fan unmanned Aerial vehicle (UAV). The UAV is capable of take-off vertically, hover and transition to cruise and is equipped with wing. the aerodynamics of the UAV is estimated through wind-tunnel experiments. The design improvement is carried out for the two phases of mission profile: hover and cruise
Pada tugas akhir ini dilakukan sebuah perancangan Pesawat Tanpa Awak (Unmanned Aerial Vehicle/ UAV)....
Engineering: 4th Place, Honorable Mention (The Ohio State University Denman Undergraduate Research F...
A proposed design for a gun-launched, unmanned aerial system (GLUAS) is presented, along with experi...
Blended wing-body (BWB) aircraft, while having good aerodynamic efficiency, is hampered with issues...
The technology of UAV (Unmanned Aerial Vehicle) has developed since its conception many years ago. U...
Our aim is to design a peculiar model on UAV which is helpful in different fields for reducing man p...
UAV development and usage has increased dramatically in the last 15 years. In this time frame the po...
Micro aerial vehicle has played more and more important rules, not only in the military. But also in...
This dissertation investigates the CM$-$SCALE Flapping Wing of Unmanned Aerial Vehicle (FWUAV) that ...
The Kenyalang-12 is an unmanned technology demonstrator aircraft equipped with a hydrogen fuel ce...
Inflatable-wing Unmanned Aerial Vehicles (UAVs) have the ability to be packed in a fraction of their...
A significant area of current research is to develop aircraft which are unmanned. More specifically,...
The drone industry yearns for enhanced aerodynamic performance. In order to achieve this feat, resea...
Aerodynamics is a branch of dynamics concerned with the study of fluid flow and the interaction of t...
This paper proposes a different innovative design of airfoils used in drones. A computational fluid ...
Pada tugas akhir ini dilakukan sebuah perancangan Pesawat Tanpa Awak (Unmanned Aerial Vehicle/ UAV)....
Engineering: 4th Place, Honorable Mention (The Ohio State University Denman Undergraduate Research F...
A proposed design for a gun-launched, unmanned aerial system (GLUAS) is presented, along with experi...
Blended wing-body (BWB) aircraft, while having good aerodynamic efficiency, is hampered with issues...
The technology of UAV (Unmanned Aerial Vehicle) has developed since its conception many years ago. U...
Our aim is to design a peculiar model on UAV which is helpful in different fields for reducing man p...
UAV development and usage has increased dramatically in the last 15 years. In this time frame the po...
Micro aerial vehicle has played more and more important rules, not only in the military. But also in...
This dissertation investigates the CM$-$SCALE Flapping Wing of Unmanned Aerial Vehicle (FWUAV) that ...
The Kenyalang-12 is an unmanned technology demonstrator aircraft equipped with a hydrogen fuel ce...
Inflatable-wing Unmanned Aerial Vehicles (UAVs) have the ability to be packed in a fraction of their...
A significant area of current research is to develop aircraft which are unmanned. More specifically,...
The drone industry yearns for enhanced aerodynamic performance. In order to achieve this feat, resea...
Aerodynamics is a branch of dynamics concerned with the study of fluid flow and the interaction of t...
This paper proposes a different innovative design of airfoils used in drones. A computational fluid ...
Pada tugas akhir ini dilakukan sebuah perancangan Pesawat Tanpa Awak (Unmanned Aerial Vehicle/ UAV)....
Engineering: 4th Place, Honorable Mention (The Ohio State University Denman Undergraduate Research F...
A proposed design for a gun-launched, unmanned aerial system (GLUAS) is presented, along with experi...