Zobrazeno 1 - 4
of 4
pro vyhledávání: '"Miodrag Milenković-Babić"'
Autor:
Mišo Prodić, Vuk Antonić, Rade Radonjić, Novak Nedić, Stevan Jovičić, Vanja Stefanović-Gobeljić, Miodrag Milenković-Babić
Publikováno v:
Scientific Technical Review. 69:32-38
Analysis of the take-off and landing distance of a single tractor propelled aircraft LASTA is presented in this paper. The purpose of the analysis is to enable certification of the LASTA aircraft according to civil regulations CS-23. The paper presen
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1a561b826d5eb7138c6adc044c9a6d8d
https://doi.org/10.5937/str1901032m
https://doi.org/10.5937/str1901032m
Autor:
Miodrag Milenković-Babić
Publikováno v:
Aircraft Engineering and Aerospace Technology. 90:1474-1478
Purpose This paper aims to present the new information about propeller thrust force contribution to airplane longitudinal stability analysis. Design/methodology/approach The method presented in this paper is empirical, shows how propeller thrust forc
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a51ed1bf4dc3014af5d9d10885eb768e
https://doi.org/10.1108/aeat-04-2017-0104
https://doi.org/10.1108/aeat-04-2017-0104
Autor:
Vanja Stefanović-Gobeljić, Miodrag Milenković-Babić, Marija Samardžić, Vuk Antonić, Milica Marjanović
Publikováno v:
Aircraft Engineering and Aerospace Technology. 89:911-919
Purpose This paper presents the longitudinal stability analysis of a single tractor propeller airplane LASTA at high engine power settings. This analysis is part of the ongoing process of certifying the airplane for civil use according to the civil r
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c6495afac468565f3b62b7082c1147a3
https://doi.org/10.1108/aeat-02-2016-0026
https://doi.org/10.1108/aeat-02-2016-0026
Publikováno v:
Aerospace Science and Technology. 46:227-235
This paper presents the analysis of effects on the airplane longitudinal stability reserve by the single tractor propeller at high engine power settings. The analysis was done within the terminal flight phases. The airplane has the original and modif
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b757b85fdfe02ef751843cc6ed50a127
https://doi.org/10.1016/j.ast.2015.07.017
https://doi.org/10.1016/j.ast.2015.07.017