Results 21 to 30 of about 14,268 (264)

Performance Analysis of Empennage Configurations on a Surveillance and Monitoring Mission of a VTOL-Plane UAV Using a Computational Fluid Dynamics Simulation

open access: yesAerospace, 2022
A Vertical Take-Off and Landing-Plane (VTOL-Plane) is an Unmanned Aerial Vehicle (UAV) that combines multirotor and fixed-wing configurations. It has a good cruise range compared to a VTOL vehicle. Furthermore, it can take-off and land vertically.
Gesang Nugroho   +2 more
doaj   +1 more source

Nonlinear similar design of large slenderness ratio truss boom

open access: yesMechanical Engineering Journal, 2017
To solve the problem that lacks systematic product spectrum plan and serialization of design methods and theoretical basis in the design process of crawler crane boom, the main boom is as the research object in this paper.
Xu-yang CAO, Peng WANG, Wen-jun WANG
doaj   +1 more source

Aerodynamic Optimization Design on Supersonic Transports Considering Sonic Boom Intensity

open access: yesXibei Gongye Daxue Xuebao, 2020
It is key points to improve the aerodynamic efficiency and decrease the sonic-boom intensity for the supersonic aircraft design. Sonic-boom prediction method with high precision combining the near-field sonic-boom prediction based on Reynolds-Averaged ...

doaj   +1 more source

Low-Boom Design for Supersonic Transport with Canard and Forward-Swept Wings Using Equivalent Area Design Method

open access: yesAerospace, 2023
Forward-swept wings can be expected to be lower-boom planforms with similar amount of drag as backward-swept wings because of their good lift distributions.
Yuki Kishi   +2 more
doaj   +1 more source

An alternative boom design and welding technique to minimize energy consumption during boom production [PDF]

open access: yesScientia Iranica, 2017
This paper presents an alternative boom design for mobile cranes and a method to produce it for minimizing the energy consumption during its production. The main change in the production of the crane booms is the shape of the booms.  Normally two symmetric boom parts are manufactured and then these parts are welded by two welding processes, in the ...
Ozcan, M., Yagci, M., Alver, V.
openaire   +2 more sources

DETERMINATION OF THE VARIED CONSTRUCTIVE PARAMETERS FOR BALANCING UNITS OF PORTAL CRANES

open access: yesNauka ta progres transportu, 2018
Purpose. The research was carried out to improve the design process of the balancing unit for portal crane. In order to achieve the purpose one should: 1) to develop a dynamic and mathematical model that allows describing the movement of balancing unit ...
V. V. Suglobov   +2 more
doaj   +1 more source

Deep learning for inverse design of low-boom supersonic configurations

open access: yesAdvances in Aerodynamics, 2023
Mitigating the sonic boom to an acceptable stage is crucial for the next generation of supersonic transports. The primary way to suppress sonic booms is to develop a low sonic boom aerodynamic shape design.
Shusheng Chen   +4 more
doaj   +1 more source

LIGHTWEIGHT DESIGN OF STRUCTURES BASED ON A SEMIDEFINITE PROGRAMMING METHOD (MT)

open access: yesJixie qiangdu, 2022
A semidefinite programming-based optimization method is proposed for lightweight design of boom and stay bars of container cranes. The boom and stay bars are welded together by steel plates, and in engineering practices the cross-sectional dimensions of ...
WANG XingFeng   +3 more
doaj  

Design of automatic control system of boom roadheader

open access: yesGong-kuang zidonghua, 2016
In view of problem of low accuracy, automation control performance and work efficiency of body positioning of existing boom roadheader, an automatic control system of boom roadheader was designed, hardware and software design of the system were ...
WANG Hong
doaj   +1 more source

Low-Boom and Low-Drag Optimization of the Twin Engine Version of Silent Supersonic Business Jet

open access: yesJournal of Fluid Science and Technology, 2008
Multi-Objective Optimization has been applied to a design problem of the twin engine concept for Silent Supersonic Business Jet (SSBJ). This problem aims to find main wing, body, tail wing and engine nacelle configurations, which can minimize both sonic ...
Koma SATO   +5 more
doaj   +1 more source

Home - About - Disclaimer - Privacy