Descriptive analysis of viability of fuel saving in commercial aircraft through the application of photovoltaic cells
This paper presents the analysis of the technical feasibility to use a photovoltaic system to
supply the electrical demand on two referential commercial aircraft, Airbus A340–300 and …
supply the electrical demand on two referential commercial aircraft, Airbus A340–300 and …
Solar-Powered UAVs: A systematic Literature Review
LS Al Dhafari, A Afzal, OK Al Abri… - 2024 2nd International …, 2024 - ieeexplore.ieee.org
Solar-powered Unmanned Aerial Vehicles (SPUAVs), commonly known as solar drones, are
an innovative and eco-friendly category of aircraft that rely on solar energy as their primary …
an innovative and eco-friendly category of aircraft that rely on solar energy as their primary …
Aerodynamic Efficiency and Performance Development in an Electric Powered Fixed Wing Unmanned Aerial Vehicle
B Kaynak, AY Arabul - Electric Power Components and Systems, 2023 - Taylor & Francis
Unmanned aerial vehicles (UAVs) have an important place in today's technologies because
of the solutions they bring to many critical problems in military and civilian application …
of the solutions they bring to many critical problems in military and civilian application …
Solar rechargeable airplane: Power system optimization
D Karabetsky - 2016 4th International Conference on Methods …, 2016 - ieeexplore.ieee.org
Solar rechargeable airplane: Power system optimization Page 1 2016 4th International
Conference on Methods and Systems of Navigation and Motion Control (MSNMC) Proceedings …
Conference on Methods and Systems of Navigation and Motion Control (MSNMC) Proceedings …
Robust functional response-based metamodel optimization considering both location and dispersion effects for aeronautical airfoil designs
M Han, L Ouyang - Structural and Multidisciplinary Optimization, 2021 - Springer
Airfoils play significant roles in aerodynamic engineering as they are important devices in
designing aircraft and engines. For airfoils, geometric design variables often deviate from …
designing aircraft and engines. For airfoils, geometric design variables often deviate from …
[引用][C] Energy system design of solar aircraft
VM Sineglazov, DP Karabetsky - 2013 IEEE 2nd International …, 2013 - ieeexplore.ieee.org
Energy system design of solar aircraft Page 1 Energy System Design of Solar Aircraft VM
Sineglazov, DP Karabetsky Aviation Computer-Integrated Complexes Department National …
Sineglazov, DP Karabetsky Aviation Computer-Integrated Complexes Department National …
[引用][C] Flying wing design for solar rechargeable aircraft
VM Sineglazov, DP Karabetsky - 2013 IEEE 2nd International …, 2013 - ieeexplore.ieee.org
Flying wing design for solar rechargeable aircraft Page 1 Flying Wing Design for Solar
Rechargeable Aircraft VM Sineglazov, DP Karabetsky Aviation Computer-Integrated …
Rechargeable Aircraft VM Sineglazov, DP Karabetsky Aviation Computer-Integrated …
[引用][C] Flying range of solar airplane
DM Karabetsky - 2015 IEEE International Conference Actual …, 2015 - ieeexplore.ieee.org
Flying range of solar airplane Page 1 2015 IEEE 3rd International Conference Actual Problems
of Unmanned Aerial Vehicles Developments (APUAVD) Proceedings pp.48-49 Flying Range …
of Unmanned Aerial Vehicles Developments (APUAVD) Proceedings pp.48-49 Flying Range …