A flight test research program employing a remotely piloted vehicle (RPV) within high angle of attack range has commenced at the Faculty of Power and Aeronautical Engineering of Warsaw University of Technology, Poland. The initial flights of the scaled model of the “Bielik” aircraft were made with the aim to correlate RPV and full‐scale flight stall and departure and spin controllability considering the effects of dynamic scaling laws and Reynolds number. The remotely controlled research aircraft, which is powered by a turbine jet engine and equipped with a flight data recording system, proved to be good source of stability and control data at relatively low cost and without additional risk. The research remotely piloted vehicle and results...
The primary objective of this thesis was to study, implement, and test low-cost electronic flight co...
The University of Glasgow, Department of Aerospace Engineering has been in possession of a Czech m...
This paper describes recent research on the design and implement of a small-scaled rotorcraft Unmann...
A flight test research program employing a remotely piloted vehicle (RPV) within high angle of attac...
Flight testing is recognised to be the definitive validation of an aerodynamic concept or of an airc...
th scale, aeroelastically equivalent Remotely Piloted Vehicle (RPV) is desired to investigate the gu...
A wind tunnel investigation of a full scale remotely piloted vehicle (RPV) armed with rocket launche...
The first four flights of a remotely piloted airplane model showed that a flight envelope can be exp...
This paper describes recent research on the design, implement and testing of a small-scaled rotorcra...
The SHARP UAS project explores a new way to achieve and test aircraft at speeds in excess of Mach on...
The thesis objective was to design an unmanned aerial vehicle that was capable of stable, autonomous...
A prototype tail-sitter mini unmanned aerial vehicle (SkyEyeV) was developed and tested in a wind tu...
This paper describes recent research on the design, implement and testing of a small-scaled rotorcra...
The paper presents building, preparing and testing of a scaled RC aerial platform, as a basis for fu...
In work, results of calculation of the main technical characteristics of the remotely - controlled a...
The primary objective of this thesis was to study, implement, and test low-cost electronic flight co...
The University of Glasgow, Department of Aerospace Engineering has been in possession of a Czech m...
This paper describes recent research on the design and implement of a small-scaled rotorcraft Unmann...
A flight test research program employing a remotely piloted vehicle (RPV) within high angle of attac...
Flight testing is recognised to be the definitive validation of an aerodynamic concept or of an airc...
th scale, aeroelastically equivalent Remotely Piloted Vehicle (RPV) is desired to investigate the gu...
A wind tunnel investigation of a full scale remotely piloted vehicle (RPV) armed with rocket launche...
The first four flights of a remotely piloted airplane model showed that a flight envelope can be exp...
This paper describes recent research on the design, implement and testing of a small-scaled rotorcra...
The SHARP UAS project explores a new way to achieve and test aircraft at speeds in excess of Mach on...
The thesis objective was to design an unmanned aerial vehicle that was capable of stable, autonomous...
A prototype tail-sitter mini unmanned aerial vehicle (SkyEyeV) was developed and tested in a wind tu...
This paper describes recent research on the design, implement and testing of a small-scaled rotorcra...
The paper presents building, preparing and testing of a scaled RC aerial platform, as a basis for fu...
In work, results of calculation of the main technical characteristics of the remotely - controlled a...
The primary objective of this thesis was to study, implement, and test low-cost electronic flight co...
The University of Glasgow, Department of Aerospace Engineering has been in possession of a Czech m...
This paper describes recent research on the design and implement of a small-scaled rotorcraft Unmann...