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Autor:
A V S N Kudryavtsev Kulikov
Publikováno v:
Vestnik Mashinostroeniya. :41-43
Failures during the landing of a light transport aircraft associated with the self-induced deployment of brake flaps are analyzed. The options for their asymmetric deployment are considered. The results of modeling the aircraft landing trajectory wit
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9b4048e621fe2e425d4889aa4e204e81
https://doi.org/10.36652/0042-4633-2021-3-41-43
https://doi.org/10.36652/0042-4633-2021-3-41-43
