Zobrazeno 1 - 10
of 111
pro vyhledávání: '"Adverse yaw"'
Publikováno v:
The Aeronautical Journal. 125:807-829
Most modern aircraft employ discrete ailerons for roll control. The induced drag, rolling moment, and yawing moment for an aircraft depend in part on the location and size of the ailerons. In the present study, lifting-line theory is used to formulat
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::fdfcf84d3f8f9b4b6af674f3b6f63f74
https://doi.org/10.1017/aer.2020.139
https://doi.org/10.1017/aer.2020.139
Publikováno v:
Defence Science Journal. 71:153-161
The implementation of interconnect gain from aileron to rudder surface on the majority of the aircraftis to decrease sideslip which is generated because of adverse yaw with the movement of control stick in lateral axis and also enhances the turning r
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::beca1c98d614888efd8afd241ecb7346
https://doi.org/10.14429/dsj.71.15347
https://doi.org/10.14429/dsj.71.15347
Publikováno v:
The Aeronautical Journal. 125:763-774
Aileron to Rudder Interconnect (ARI) gain is implemented on most fighter aircraft, primarily to reduce the side slip produced due to adverse yaw from pilot lateral control stick input and to improve the turn rate response. A systematic and non-iterat
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::06a3840fc72c709a40319de394a9195d
https://doi.org/10.1017/aer.2020.131
https://doi.org/10.1017/aer.2020.131
Publikováno v:
AIAA Journal. 58:2909-2920
Lifting-line theory has formed the basis of wing-design understanding for nearly a century. This theory has previously been used to develop a class of optimal lift distributions that minimize induc...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5f8a0a888fc12330aa1e5e87dd3fc9c6
https://doi.org/10.2514/1.j059038
https://doi.org/10.2514/1.j059038
Publikováno v:
Journal of Aircraft. 57:603-614
Flying wings achieve their roll, pitch, and yaw controllability exclusively through spanwise variations of lift and drag due to the lack of an empennage. Instead of using conventional control surfa...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4fe7b6c3045efc9c45e7c32a74358d26
https://doi.org/10.2514/1.c035606
https://doi.org/10.2514/1.c035606
Autor:
Montgomery, Zachary S.
Publikováno v:
All Graduate Theses and Dissertations
Advanced aircraft designs tend to have several control surfaces or devices that affect the flight of the aircraft. It is difficult or even impossible for a pilot to directly control each of these devices and fly the aircraft well. Therefore, a contro
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::f8487f7aea42bf540abee75cb73ee0f9
Autor:
Snorri Gudmundsson
Publikováno v:
General Aviation Aircraft Design ISBN: 9780128184653
The chapter presents a number of important topics that do not belong to any particular one of the preceding ones, but rather a number of them. It begins with a presentation of various requirements for control surface design. It also details a method
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::ba0078e3824a54641de85aa662975ad3
https://doi.org/10.1016/b978-0-12-818465-3.00026-4
https://doi.org/10.1016/b978-0-12-818465-3.00026-4
Autor:
Henningsson, P., Johansson, L. C.
Publikováno v:
Journal of the Royal Society Interface
For all flyers, aeroplanes or animals, making banked turns involve a rolling motion which, due to higher induced drag on the outer than the inner wing, results in a yawing torque opposite to the turn. This adverse yaw torque can be counteracted using
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::16f8b53fca10d33fa86183d30113ea47
https://doi.org/10.1098/rsif.2021.0779
https://doi.org/10.1098/rsif.2021.0779
Publikováno v:
ZAMM - Journal of Applied Mathematics and Mechanics / Zeitschrift für Angewandte Mathematik und Mechanik. 101
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8e259aff4a147fcb2adc85f98eff7a7c
https://doi.org/10.1002/zamm.201900177
https://doi.org/10.1002/zamm.201900177
Akademický článek
Tento výsledek nelze pro nepřihlášené uživatele zobrazit.
K zobrazení výsledku je třeba se přihlásit.
K zobrazení výsledku je třeba se přihlásit.