In this project, by analyzing different airfoils the suitable airfoil which has less camber for solar cell placement was chosen by XFLR5 analysis. With this airfoil, the wing span and chord was decided according to the battery requirement. Then energy and power analysis was done theoretically to check the design feasibility, which gives a basic foundation in order to design a solar-powered UAV. Then the integration of solar cells on to the wing was performed by considering various factors such as the deflection, stability and circuit connectivity. Then the solar wing was tested and from the solar cells, more than the required power for the level flight has been obtained, which shows that with this power the plane can fly with only solar energy continuously for more than 6 hours. And for the designed prototype the thermodynamic analysis of solar PV cells was performed taking into account the effect of temperature along with the wind. Then finally the exergy analysis has been done in order to provide a physical basis for understanding, refining and predicting the variations in solar PV behavior.
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In this project, by analyzing different airfoils the suitable airfoil which has less camber for solar cell placement was chosen by XFLR5 analysis. With this airfoil, the wing span and chord was decided according to the battery requirement. Then energy and power analysis was done theoretically to check the design feasibility, which gives a basic foundation in order to design a solar-powered UAV. Then the integration of solar cells on to the wing was performed by considering various factors such as the deflection, stability and circuit connectivity. Then the solar wing was tested and from the solar cells, more than the required power for the level flight has been obtained, which shows that with this power the plane can fly with only solar energy continuously for more than 6 hours. And for the designed prototype the thermodynamic analysis of solar PV cells was performed taking into account the effect of temperature along with the wind. Then finally the exergy analysis has been done in order to provide a physical basis for understanding, refining and predicting the variations in solar PV behavior.
B.S Karthik has completed his Bachelor's degree in Mechanical Engineering from Vellore Institute of Technology, India in 2016. After that, he started working in IDMC company which is an energy audit and manufacturing company. In future, he was planning to do Master's in Renewable Energy Engineering in Germany to curtail the rising energy demands.
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Taschenbuch. Zustand: Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -In this project, by analyzing different airfoils the suitable airfoil which has less camber for solar cell placement was chosen by XFLR5 analysis. With this airfoil, the wing span and chord was decided according to the battery requirement. Then energy and power analysis was done theoretically to check the design feasibility, which gives a basic foundation in order to design a solar-powered UAV. Then the integration of solar cells on to the wing was performed by considering various factors such as the deflection, stability and circuit connectivity. Then the solar wing was tested and from the solar cells, more than the required power for the level flight has been obtained, which shows that with this power the plane can fly with only solar energy continuously for more than 6 hours. And for the designed prototype the thermodynamic analysis of solar PV cells was performed taking into account the effect of temperature along with the wind. Then finally the exergy analysis has been done in order to provide a physical basis for understanding, refining and predicting the variations in solar PV behavior. 52 pp. Englisch. Bestandsnummer des Verkäufers 9783330090101
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Zustand: New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. Autor/Autorin: Reddy B.S KarthikB.S Karthik has completed his Bachelor s degree in Mechanical Engineering from Vellore Institute of Technology, India in 2016. After that, he started working in IDMC company which is an energy audit and manufacturing. Bestandsnummer des Verkäufers 509614548
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Taschenbuch. Zustand: Neu. Neuware -In this project, by analyzing different airfoils the suitable airfoil which has less camber for solar cell placement was chosen by XFLR5 analysis. With this airfoil, the wing span and chord was decided according to the battery requirement. Then energy and power analysis was done theoretically to check the design feasibility, which gives a basic foundation in order to design a solar-powered UAV. Then the integration of solar cells on to the wing was performed by considering various factors such as the deflection, stability and circuit connectivity. Then the solar wing was tested and from the solar cells, more than the required power for the level flight has been obtained, which shows that with this power the plane can fly with only solar energy continuously for more than 6 hours. And for the designed prototype the thermodynamic analysis of solar PV cells was performed taking into account the effect of temperature along with the wind. Then finally the exergy analysis has been done in order to provide a physical basis for understanding, refining and predicting the variations in solar PV behavior.Books on Demand GmbH, Überseering 33, 22297 Hamburg 52 pp. Englisch. Bestandsnummer des Verkäufers 9783330090101
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Taschenbuch. Zustand: Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - In this project, by analyzing different airfoils the suitable airfoil which has less camber for solar cell placement was chosen by XFLR5 analysis. With this airfoil, the wing span and chord was decided according to the battery requirement. Then energy and power analysis was done theoretically to check the design feasibility, which gives a basic foundation in order to design a solar-powered UAV. Then the integration of solar cells on to the wing was performed by considering various factors such as the deflection, stability and circuit connectivity. Then the solar wing was tested and from the solar cells, more than the required power for the level flight has been obtained, which shows that with this power the plane can fly with only solar energy continuously for more than 6 hours. And for the designed prototype the thermodynamic analysis of solar PV cells was performed taking into account the effect of temperature along with the wind. Then finally the exergy analysis has been done in order to provide a physical basis for understanding, refining and predicting the variations in solar PV behavior. Bestandsnummer des Verkäufers 9783330090101
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Taschenbuch. Zustand: Neu. Experimental Analysis on Solar Powered Unmanned Aerial Vehicle | The design of Solar Plane. | B. S Karthik Reddy (u. a.) | Taschenbuch | Englisch | 2017 | LAP LAMBERT Academic Publishing | EAN 9783330090101 | Verantwortliche Person für die EU: preigu GmbH & Co. KG, Lengericher Landstr. 19, 49078 Osnabrück, mail[at]preigu[dot]de | Anbieter: preigu Print on Demand. Bestandsnummer des Verkäufers 120563787
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