Zobrazeno 1 - 10
of 215
pro vyhledávání: '"elevon"'
Autor:
D. V. Elenin
Publikováno v:
System analysis and logistics. 2:26-32
The article discusses the possibility of creating two schemes of an experimental control body in flight for a UAV of the "Flying Wing" scheme. The concept of creating a real prototype for an experiment in the Solidworks Flow environment and in a wind
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6f216ba6bc1b6549c3cf372136bb687b
https://doi.org/10.31799/2077-5687-2021-2-26-32
https://doi.org/10.31799/2077-5687-2021-2-26-32
Autor:
Raghvendra Gautam, Ashutosh Kumar
Objectives: To study a hybrid VTOL- Blended wing body design for its wings and elevons and perform CFD simulations with the wings. The steps for designing wing configuration and Elevon positioning involve different variables giving rise to a large nu
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::63cd42cd156567e5fa99f953d8f3e4c7
https://zenodo.org/record/5526099
https://zenodo.org/record/5526099
Publikováno v:
Materials Today: Proceedings. 26:2895-2900
The material selection and designing for a shape-changing airfoil and actuated elevon mechanism to improve endurance, payload, flight trajectories, and mechanical-failure is presented. The selection of the active, expands on heating, and passive laye
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9f8d5847187f8ec8653bc2dfbc5f66e6
https://doi.org/10.1016/j.matpr.2020.02.598
https://doi.org/10.1016/j.matpr.2020.02.598
Autor:
A. A. Krivoshchapov
Publikováno v:
Russian Aeronautics. 62:342-347
The results are given on the experimental studies of integral aerodynamic characteristics of X-47B-type “flying wing” unmanned aerial vehicle model. The dependence of the lift coefficient on the angle of attack for different trimmings and static
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::dd7fed2b28bac38a352d727d8ed9ff41
https://doi.org/10.3103/s1068799819020247
https://doi.org/10.3103/s1068799819020247
Publikováno v:
CEAS Aeronautical Journal 12(4), 895-906 (2021). doi:10.1007/s13272-021-00545-3
CEAS Aeronautical Journal 12(4), 895-906 (2021). doi:10.1007/s13272-021-00545-3
Published by Springer, Wien [u.a.]
Published by Springer, Wien [u.a.]
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::b1eabf4568ae7922504b5a25f4ce0904
https://publications.rwth-aachen.de/record/842577
https://publications.rwth-aachen.de/record/842577
Publikováno v:
Lecture Notes in Mechanical Engineering ISBN: 9789811596001
This paper presents the details about lateral-directional and longitudinal control of a tailless aircraft for landing condition. Tailless aircraft configurations are specifically designed for stealth and the absence of a vertical fin aids in low visi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::15c56f0688e5039416ec403333716de1
https://doi.org/10.1007/978-981-15-9601-8_40
https://doi.org/10.1007/978-981-15-9601-8_40
Publikováno v:
2020 3rd International Conference on Unmanned Systems (ICUS).
Effects of aeroelastic deformation on control surface efficiency of a flying wing aircraft are investigated using CFD/CSD coupling method. Results indicate that the equivalent deflection angles of inboard elevon, outboard elevon and split rudder decr
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::84e6ff1f7af891a7a18b097499eeb14b
https://doi.org/10.1109/icus50048.2020.9274846
https://doi.org/10.1109/icus50048.2020.9274846
Publikováno v:
Lecture Notes in Civil Engineering ISBN: 9783030551148
Modern aircraft structures uses more lightweight materials such as composites for their design. This makes the aeroelastic study an extremely important aspect of aircraft design. By having more light weight control surfaces, the control effectiveness
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0991ecfef04d10ae19a78e9c7f00ff1b
https://doi.org/10.1007/978-3-030-55115-5_21
https://doi.org/10.1007/978-3-030-55115-5_21
Publikováno v:
AIAA AVIATION 2020 FORUM.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d07f2310b9d20e07d6c9632f2890d933
https://doi.org/10.2514/6.2020-3008
https://doi.org/10.2514/6.2020-3008
Publikováno v:
Journal of Intelligent Material Systems and Structures. 29:3847-3872
Tailless airplanes with swept wings rely on variations of the spanwise lift distribution to provide controllability in roll, pitch and yaw. Conventionally, this is achieved utilizing multiple control surfaces, such as elevons, on the wing trailing ed
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::e2b806972d631e3790405415971d0a75
https://doi.org/10.1177/1045389x18798952
https://doi.org/10.1177/1045389x18798952