Zobrazeno 1 - 4
of 4
pro vyhledávání: '"Shashank Maurya"'
Autor:
Mahesh S Patil, Satyadhyan Chickerur, C Abhimalya, Anishma Naik, Nidhi Kumari, Shashank Maurya
Publikováno v:
Procedia Computer Science. 218:1156-1165
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0e27e5d02b268ff644912552a59457dc
https://doi.org/10.1016/j.procs.2023.01.094
https://doi.org/10.1016/j.procs.2023.01.094
Publikováno v:
Journal of Aircraft. 58:153-166
In forward flight, slowing down a rotor alleviates compressibility effects on the advancing side blade tip, extending the cruise speed limit, and inducing high-advance-ratio flight regime. Previous...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3a3f60f91f06439d8e3a610669d4a5d2
https://doi.org/10.2514/1.c035900
https://doi.org/10.2514/1.c035900
Publikováno v:
2021 5th International Conference on Information Systems and Computer Networks (ISCON).
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1e1d64f54c96427e20bca2b558db8dc8
https://doi.org/10.1109/iscon52037.2021.9702301
https://doi.org/10.1109/iscon52037.2021.9702301
Publikováno v:
Journal of the American Helicopter Society.
A single main rotor helicopter's maximum forward speed is limited due to the compressibility effects on the advancing side and reverse flow and dynamic stall on the retreating side. Compound helicopters can address these issues with a slowed rotor an
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::eb14fb72dcf37decc835648cee58c5aa
https://doi.org/10.4050/jahs.66.042005
https://doi.org/10.4050/jahs.66.042005