Zobrazeno 1 - 10
of 13
pro vyhledávání: '"Maria E. Sidoryuk"'
Publikováno v:
IFAC-PapersOnLine. 52:526-531
The paper presents a technique for cost-effective and safe study of conventional and critical flight regimes and control validation using an autonomous dynamically scaled aircraft model mounted in a three-degree-of-freedom gimbal in a wind tunnel. Th
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::74a0118626d004fe322cd730a488a7bc
https://doi.org/10.1016/j.ifacol.2019.11.297
https://doi.org/10.1016/j.ifacol.2019.11.297
Publikováno v:
Journal of Aircraft. 56:205-216
Aircraft spin susceptibility is a critical parameter for the flight safety. Recently developed quantitative methods for analysis of nonlinear systems are applied to analysis of aircraft spins. The ...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d4618d1b5555366fcc22ce474af6ca5a
https://doi.org/10.2514/1.c034936
https://doi.org/10.2514/1.c034936
Autor:
Diana Aleksandrovna Alieva, A. I. Kortukova, Maria E. Sidoryuk, Dmitry I. Ignatyev, Sergey G. Bazhenov, Alexander N. Khrabrov
Airframe icing causes significant degradation of aerodynamic characteristics and influences the flight safety. Wind tunnel study of longitudinal steady and unsteady aerodynamic characteristics of a transport aircraft in icing conditions is carried ou
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::a492121e32c04cd1570b1361f2cc681d
https://dspace.lib.cranfield.ac.uk/handle/1826/15520
https://dspace.lib.cranfield.ac.uk/handle/1826/15520
Publikováno v:
Journal of Aircraft
Journal of Aircraft, American Institute of Aeronautics and Astronautics, 2020, pp.1-16. ⟨10.2514/1.C035882⟩
Journal of Aircraft, American Institute of Aeronautics and Astronautics, 2020, pp.1-16. ⟨10.2514/1.C035882⟩
International audience; Reliable prediction of aircraft post-stalled dynamics is entirely dependent on the adequacy of the aerodynamic model. A mathematical model of aerodynamic characteristics of a light aircraft is developed for a wide range of ang
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::df67967dbe914c89c32f55e1a66093a5
https://hal.archives-ouvertes.fr/hal-02475981v2/document
https://hal.archives-ouvertes.fr/hal-02475981v2/document
Publikováno v:
TsAGI Science Journal. 49:77-92
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::fdf36281f60fc87391570615d4b3d8d6
https://doi.org/10.1615/tsagiscij.2018026767
https://doi.org/10.1615/tsagiscij.2018026767
Autor:
Konstantin Anatolievich Kolinko, Maria E. Sidoryuk, Alexander N. Khrabrov, Dmitry I. Ignatyev
Publikováno v:
Journal of Aircraft. 54:1760-1771
The dynamics of a modern aircraft at high angles of attack is complicated, with hazardous phenomena such as wing rock, stall, and spin. The paper presents a technique for cost-effective and safe st...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2c218c69a0ff0c615efd6a9b6017d52b
https://doi.org/10.2514/1.c034167
https://doi.org/10.2514/1.c034167
ON POSSIBILITY OF CRITICAL FLIGHT REGIME STUDY IN WIND TUNNELS USING THREE-DEGREE-OF-FREEDOM GIMBALS
Autor:
Evgueniy Nikolaevich Kolesnikov, Konstantin Anatolievich Kolinko, Yuriy Alexandrovich Vinogradov, Alexander N. Khrabrov, Maria E. Sidoryuk, Igor Igorevich Grishin
Publikováno v:
TsAGI Science Journal. 45:825-839
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7540c11011548dc2cee59854b343329a
https://doi.org/10.1615/tsagiscij.2015013365
https://doi.org/10.1615/tsagiscij.2015013365
Autor:
Alexander N. Khrabrov, Kamil G. Zaripov, Maria E. Sidoryuk, Dmitry I. Ignatyev, Konstantin Anatolievich Kolinko
Publikováno v:
AIAA Atmospheric Flight Mechanics Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::48f6cff8f58501b7ef6c677ae66beae3
https://doi.org/10.2514/6.2016-3106
https://doi.org/10.2514/6.2016-3106
The aerodynamic model of a generic airliner configuration is developed for a wide range of angles of attack, sideslip and angular rate based on experimental data obtained in wind tunnels using static, forced oscillations and rotary balance tests. The
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::843494653051dff5542f99c5381e5fdc
http://hdl.handle.net/2086/9104
http://hdl.handle.net/2086/9104
Publikováno v:
Scopus-Elsevier
A systematic investigation of aircraft equilibrium states and their local stability characteristics is used for clearance of flight control laws for a large variety of manoeuvres. The proposed approach is illustrated by clearance of the LPV control l
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::58dac8457bfe44da6faaa0dd2801981f
http://hdl.handle.net/2086/9101
http://hdl.handle.net/2086/9101