AbstractUltra-light and very light amphibious aircrafts are the special kinds of low-speed general aircrafts. They are low weighted and small sized but can takeoff and land either on land or water without changing the structure of any parts. These characteristics result in the distinctive configuration and structure design, and meanwhile bring about significant features of safety and airworthiness design. These problems are investigated by developing the ultra-light amphibious aircraft “Frigate bird” and analyzing the other aircrafts’ design. This paper mainly discusses the preliminary design about structure, aerodynamics, power effect, flying qualities, dynamics and statics on water. Some analysis methodologies and design parameters which ...
The paper describes the optimization of the hull of the Idintos PrandPlane obtained by means of CFD ...
This paper presents the design and development of an Autonomous Amphibious Unmanned Aerial Vehicle (...
This paper describes a systematic technique for preliminary conceptual design of Unmanned Wing in Gr...
Due to the outstanding take-off and landing advantages and multiple application fields, amphibious a...
This paper describes the preliminary CFD analyses of a ultralight amphibious PrandtlPlane, performed...
The paper deals with the activities to design and manufactoring a prototype of a PrandtlPlane aircra...
Unmanned Amphibious Aerial Vehicles (UAAV) are gaining significant interest in accessing remote wate...
The design of a PrandtlPlane amphibian is based on aerodynamic optimization, CFD simulations and al...
This article’s incitement interprets Unmanned Amphibious Aerial Vehicle (UAAV)’s conceptual design p...
The IDINTOS project, co-founded by the Regional Government of Tuscany (Italy), concerns the design o...
This master thesis is involved in the IDINTOS project, and in particular it studies the preliminary ...
This study is laid out in 8 self-explanatory sections. The Introduction sets the scene for the thes...
The design and analysis of a new airfoil to be employed on a ultralight aircraft with short takeoff ...
This thesis addresses the design of ultralight aircraft as a one regulation UL-2 and basic aerodynam...
The class of ULM (Ultra Light Machines) and light aircraft in general has attracted growing interest...
The paper describes the optimization of the hull of the Idintos PrandPlane obtained by means of CFD ...
This paper presents the design and development of an Autonomous Amphibious Unmanned Aerial Vehicle (...
This paper describes a systematic technique for preliminary conceptual design of Unmanned Wing in Gr...
Due to the outstanding take-off and landing advantages and multiple application fields, amphibious a...
This paper describes the preliminary CFD analyses of a ultralight amphibious PrandtlPlane, performed...
The paper deals with the activities to design and manufactoring a prototype of a PrandtlPlane aircra...
Unmanned Amphibious Aerial Vehicles (UAAV) are gaining significant interest in accessing remote wate...
The design of a PrandtlPlane amphibian is based on aerodynamic optimization, CFD simulations and al...
This article’s incitement interprets Unmanned Amphibious Aerial Vehicle (UAAV)’s conceptual design p...
The IDINTOS project, co-founded by the Regional Government of Tuscany (Italy), concerns the design o...
This master thesis is involved in the IDINTOS project, and in particular it studies the preliminary ...
This study is laid out in 8 self-explanatory sections. The Introduction sets the scene for the thes...
The design and analysis of a new airfoil to be employed on a ultralight aircraft with short takeoff ...
This thesis addresses the design of ultralight aircraft as a one regulation UL-2 and basic aerodynam...
The class of ULM (Ultra Light Machines) and light aircraft in general has attracted growing interest...
The paper describes the optimization of the hull of the Idintos PrandPlane obtained by means of CFD ...
This paper presents the design and development of an Autonomous Amphibious Unmanned Aerial Vehicle (...
This paper describes a systematic technique for preliminary conceptual design of Unmanned Wing in Gr...