Results 21 to 30 of about 10,974 (193)

Wing Structural Model for Overall Aircraft Design of Distributed Electric Propulsion General Aviation and Regional Aircraft

open access: yesAerospace, 2021
In the context of reducing the environmental footprint of tomorrow’s aviation, Distributed Electric Propulsion (DEP) has become an increasingly interesting concept.
Raquel Alonso Castilla   +3 more
doaj   +1 more source

Propulsion of a Molecular Machine by Asymmetric Distribution of Reaction Products [PDF]

open access: yesPhysical Review Letters, 2005
A simple model for the reaction-driven propulsion of a small device is proposed as a model for (part of) a molecular machine in aqueous media. Motion of the device is driven by an asymmetric distribution of reaction products. The propulsive velocity of the device is calculated as well as the scale of the velocity fluctuations.
Golestanian, Ramin   +2 more
openaire   +6 more sources

A laminar flow, propulsive, jet-flapped concept for electrically powered transport aircraft

open access: yesAviation, 2023
Friction drag constitutes approximately half of the total drag of subsonic civil transport aircraft at cruise conditions. Several means were examined to control the flow over an aircraft and achieve laminar flow.
Nikolaos Kehayas
doaj   +1 more source

A contribution to the investigation of acoustic interferences in aircraft distributed propulsion [PDF]

open access: yesCEAS Aeronautical Journal, 2023
AbstractThe objective of this work is to better understand the acoustic interferences created by distributed propulsion engines based on an approach that combines RANS simulation results for the aerodynamic prediction and analytical models to calculate acoustics. A multi-propeller configuration without wing is considered for this investigation.
Sébastien Guérin, Damiano Tormen
openaire   +1 more source

Aero-Propulsive Interactions between UAV Wing and Distributed Propellers Due to Their Relative Position

open access: yesDrones, 2023
The purpose of this paper is the evaluation of the aero-propulsive effects on a UAV wing model with distributed propulsion. An array of three propellers is placed ahead of the leading edge of a rectangular wing with flap.
Danilo Ciliberti   +3 more
doaj   +1 more source

Aerodynamics and Power Balance of a Distributed Aft-Fuselage Boundary Layer Ingesting Aircraft

open access: yesAerospace, 2023
This paper presents a first investigation into the aerodynamics and performance breakdown of a distributed aft-fuselage boundary layer ingesting (BLI) tube-and-wing aircraft using fully coupled Unsteady Reynolds-Averaged Navier-Stokes (URANS ...
Tze Sing Tse, Cesare A. Hall
doaj   +1 more source

Numerical investigation of aerodynamic effects of distributed propulsion [PDF]

open access: yes, 2022
The concept of distributed propulsion is to integrate the propulsion system with the airframe to exploit synergies of such a configuration. This report describes a CFD study of the aerodynamic effect of distributed propulsion.
Toniato, Pierpaolo
core  

Traction Amplified Actuation System for Inspecting Narrow and Complex Pipes Using Enhanced Linear Antagonistic Mechanism-Bend Pipe Passage Model and Force Comparison

open access: yesIEEE Access, 2023
This paper describes the design, experiments, and quantitative force comparison of a Pipe Inspection RObot named PI-RO II using the enhanced linear antagonistic mechanism to amplify the traction.
F. Ito   +4 more
doaj   +1 more source

Untethered Flight of a 270 mg Microrobot Powered by Onboard Energy

open access: yesAdvanced Intelligent Systems, 2023
It is challenging for microrobots to fly using onboard energy due to the relatively heavy power supplies and inefficient actuators that are limited to a small size (mass less than 1000 mg and wingspan less than 100 mm).
RuiDe Yun   +7 more
doaj   +1 more source

Influences of distributed propulsion system parameters on aerodynamic characteristics of a BLI-BWB UAV

open access: yesXibei Gongye Daxue Xuebao, 2021
Focusing on the aerodynamic characteristics of the blended wing body (BWB) aircraft with boundary layer ingestion(BLI) distributed propulsion system; the influences of propulsion system parameters under the condition of cruise and takeoff are studied ...

doaj   +1 more source

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