Add to ORKGThis master's thesis is focused on conceptual design of glider with electric propulsion system following the CS-22 regulation. Statistical analysis of the glider with an auxiliary electric engine has been carried out in order to determine basic design parameters for conceptual design. Based on analytical drag polar, the flight performance parameters are calculated, in particular flight range and influence of the solar panels on the flight range. This thesis also includes preliminary design solution of accumulator placement within the wing
The paper describes the selection of a distributed propulsion for the AOS H2 motor glider (selection...
Analysis of the possibility of using an engine with a rotating piston as the propulsion of an electr...
This thesis investigates the viability of creating a fully electrical motorsystem for a large UAV ca...
Diplomová práce se věnuje koncepčnímu návrhu kluzáku s elektrickým pohonem dle předpisu CS-22. Je zp...
This thesis is focused on conceptual design of electric powered training aircraft, using certificati...
The aim of this thesis was the design of a retractable, electric propulsion system for sailplanes, w...
Thesis treats influences of geometrical characteristics on aerodynamic wing properties generally mea...
This master thesis is focused on aerodynamic design of transonic glider, which is assigned for follo...
The master’s thesis deals with conceptual design of a new electrically powered aircraft as assignmen...
Unmanned Aerial Vehicles have seen an unprecedented growth in recent years in both military as well ...
In sailplane aviation, I attach great importance to the achieved aerodynamic parameters due to the m...
The objective of this work is to adopt and further expand the type design of the SONG motor glider. ...
The diploma thesis deals with the issue of electric and hybrid aircraft propulsion. The first part o...
Tato diplomová práce se zabývá návrhem remotorizace motorizovaného kluzáku L-13 Vivat elektrickým po...
The aim of the study is to design a HALE UAV using both turbofan engine and solar energy in order to...
The paper describes the selection of a distributed propulsion for the AOS H2 motor glider (selection...
Analysis of the possibility of using an engine with a rotating piston as the propulsion of an electr...
This thesis investigates the viability of creating a fully electrical motorsystem for a large UAV ca...
Diplomová práce se věnuje koncepčnímu návrhu kluzáku s elektrickým pohonem dle předpisu CS-22. Je zp...
This thesis is focused on conceptual design of electric powered training aircraft, using certificati...
The aim of this thesis was the design of a retractable, electric propulsion system for sailplanes, w...
Thesis treats influences of geometrical characteristics on aerodynamic wing properties generally mea...
This master thesis is focused on aerodynamic design of transonic glider, which is assigned for follo...
The master’s thesis deals with conceptual design of a new electrically powered aircraft as assignmen...
Unmanned Aerial Vehicles have seen an unprecedented growth in recent years in both military as well ...
In sailplane aviation, I attach great importance to the achieved aerodynamic parameters due to the m...
The objective of this work is to adopt and further expand the type design of the SONG motor glider. ...
The diploma thesis deals with the issue of electric and hybrid aircraft propulsion. The first part o...
Tato diplomová práce se zabývá návrhem remotorizace motorizovaného kluzáku L-13 Vivat elektrickým po...
The aim of the study is to design a HALE UAV using both turbofan engine and solar energy in order to...
The paper describes the selection of a distributed propulsion for the AOS H2 motor glider (selection...
Analysis of the possibility of using an engine with a rotating piston as the propulsion of an electr...
This thesis investigates the viability of creating a fully electrical motorsystem for a large UAV ca...