Journal
AEROSPACE SCIENCE AND TECHNOLOGY
Volume 108, Issue -, Pages -Publisher
ELSEVIER FRANCE-EDITIONS SCIENTIFIQUES MEDICALES ELSEVIER
DOI: 10.1016/j.ast.2020.106404
Keywords
Wingtip connection; Solar aircraft; Energy consumption; Flight endurance; Number of connected solar aircraft; Maximum flight latitude
Categories
Funding
- National Natural Science Foundation of China [11902156, 11672133]
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This study investigates the effects of wingtip connection on reducing energy consumption and increasing flight endurance for solar aircraft. The results show that wingtip connection design can effectively decrease induced drag coefficient, increase flight endurance and range, especially with higher solar cell efficiency and more connected solar aircrafts.
This study explores the effects of wingtip connection on decreasing energy consumption and increasing flight endurance for solar aircraft. The Oswald efficiency factor, induced drag coefficient and power consumption are derived as the models of the number of wingtip connected aircraft. As the energy margin model is related to the number of connected solar aircraft, a flight endurance margin model is proposed to evaluate the advantages of wingtip connection quantitatively. With the numerical method developed, researches on the energy and flight endurance performance for a given example wingtip-connected solar aircraft are performed. Moreover, the impacts of solar cell efficiency, flight date and latitude on the advantages of wingtip connection for solar aircraft are explored. The results suggest that the wingtip connection design enables solar aircraft to decrease induced drag coefficient, increase flight endurance and range effectively when the aircraft is only powered by battery. The wingtip connection design is more effective to increase the flight endurance and improve the maximum perpetual flight latitude with more connected solar aircrafts and higher solar cell efficiency, especially in the flight condition with high solar elevation angle and more daylight hours. However, as the number of connected solar aircraft increases, the effect of one more connected aircraft on these advantages decreases because the effect of wingtip connection on decreasing induced drag coefficient decreases with increasing aspect ratio. (C) 2020 Elsevier Masson SAS. All rights reserved.
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