Zobrazeno 1 - 10 of 88 pro vyhledávání: '"Closed wing"'
1
An Annular Wing VTOL UAV: Flight Dynamics and Control
Autor: Raffaello D'Andrea, Rajan Gill
Publikováno v: Drones, 4 (2)
Drones, Vol 4, Iss 14, p 14 (2020)
Drones
Volume 4
Issue 2
A vertical takeoff and landing, unmanned aerial vehicle is presented that features a quadrotor design for propulsion and attitude stabilization, and an annular wing that provides lift in forward flight. The annular wing enhances human safety by enshr
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::31462eff5067f6d7adc12066d7737250
https://hdl.handle.net/20.500.11850/414501
Zobrazit plný text záznamu
4
Determination of Gas-Generator Fuel Capacity for Hybrid Aerial Underwater Vehicles with Airfoil Cavity-Forming System
Autor: V. A. Sorokin, V. P. Makhrov, A. I. Yur’ev
Publikováno v: Russian Aeronautics. 60:495-499
We determine the behavior of onboard gas-generator flowrate for generating the cavitation flow around a hybrid aerial underwater vehicle by using an annular wing on the underwater trajectory section.
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::4bc69b6ed4310f2c46afa568e1b1ad3a
https://doi.org/10.3103/s1068799817040031
Zobrazit plný text záznamu
6
Aerodynamic Investigation on a Novel Paper-Folding Micro Annular Aerial Robot
Autor: Feng Xiaoyu, Bai Junqiang, Min Chang, Yu Zheng
Publikováno v: 2019 4th International Conference on Robotics and Automation Engineering (ICRAE).
Micro aerial vehicle (MAV) gradually gains plentiful attention in recent years. However, it is still a full challenge to design MAVs with high aerodynamic performance because aerodynamic efficiency of wings deteriorates sharply at low Reynolds number
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::3be32c653b7d0dabe212b0132c911aba
https://doi.org/10.1109/icrae48301.2019.9043792
Zobrazit plný text záznamu
7
Control of a swept wing tailless aircraft through wing morphing
Autor: Richard W. Guiler
Inspired by flight in nature, the work done by Lippisch, the Hortens, and Northrop offered insight to achieving the efficiency of bird flight with swept-wing tailless aircraft. Tailless designs must incorporate aerodynamic compromises for control, wh
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::9f38ff9e56523ed9a4efdb158b7f7259
https://doi.org/10.33915/etd.2779
Zobrazit plný text záznamu
9
On the wing density and the inflation factor of aircraft
Autor: Geoffrey R. Spedding, Leandi Liebenberg, Edward Henry Mathews, R. J. Huyssen
Publikováno v: The Aeronautical Journal. 120:291-312
The aviation industry is dominated by the domain of heavier-than-air, fixed-wing, subsonic flight, and central to any design in this domain is the wing itself. One of the earliest debates in aviation still centres around the usefulness of the wing vo
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::f501a510832cc425a0215a0c794d2216
https://doi.org/10.1017/aer.2015.12
Zobrazit plný text záznamu
10
STUDY OF THE INFLUENCE OF A GAP BETWEEN THE WING AND SLOTTED FLAP ON THE AERODYNAMIC CHARACTERISTICS OF ULTRA-LIGHT AIRCRAFT WING AIRFOIL
Autor: Michael Todorov, Cvetelina Velkova
Publikováno v: Review of the Air Force Academy. 13:39-44
The purpose of the study is to assess what the influence of the distance of the gap is between the wing and slotted flap on the aerodynamic characteristics of ultra-light aircraft wing when the flap is retracted. It has been elected numerical approac
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::1ae317edda03fd06295a16c6796950bb
https://doi.org/10.19062/1842-9238.2015.13.3.6
Zobrazit plný text záznamu

Vyhledávací nástroje:

Upřesnit hledání

Omezení vyhledávání
Plný text Recenzováno Digitální knihovna AV ČR
Zdroje