Results 41 to 50 of about 10,974 (193)

Hydrodynamic Assessment of Distributed Propulsion Systems for Shallow-Draft Inland Vessels

open access: yesPolish Maritime Research
This study investigates the hydrodynamic performance of three distributed propulsion configurations with distinct hull shapes. The influence of duct design and hull geometry on thrust, absorbed power, and the resulting thrust-to-power ratio is explored ...
Jurkovic Martin   +5 more
doaj   +1 more source

Design of distributed propulsion system for general aviation airplane [PDF]

open access: yesMATEC Web of Conferences, 2019
In this paper, a small airplane is redesigned by using a distributed electrical propulsion (DEP) system. The design procedure is focused on the reduction of fuel consumption in cruise regime with constrained parameters of take-off/landing.
Hospodář Pavel   +2 more
doaj   +1 more source

Influence of Electric Wing Tip Propulsion on the Sizing of the Vertical Stabilizer and Rudder in Preliminary Aircraft Design

open access: yesAerospace, 2023
During preliminary aircraft design, the vertical tail sizing is conventionally conducted by the use of volume coefficients. These represent a statistical approach using existing configurations’ correlating parameters, such as wing span and lever arm, to ...
Alexander Albrecht   +5 more
doaj   +1 more source

Trends in Flight-Operated Small-Satellite Propulsion Technologies

open access: yesApplied Sciences
The development and execution of prospective inner and outer space missions require focusing on the use of many small space vehicles operating in swarms with multiple informational, navigational, and mission-oriented interactions among themselves.
Andrei Shumeiko   +3 more
doaj   +1 more source

Propulsion System for BWB Configurations in the Agile project

open access: yes, 2018
The focus of the present paper is the preliminary design of the propulsion and on-board systems and their integration for a Blended Wing Body (BWB) aircraft.
Luca Boggero   +13 more
core   +1 more source

The Impact of Distributed Propulsion on the Aerodynamic Characteristics of a Blended-Wing-Body Aircraft

open access: yesAerospace, 2022
Motivated by outstanding aerodynamic performance and limited emissions, the blend-wing-body (BWB) aircraft equipped with a distributed propulsion (DP) system has become a possible layout for civil aircraft in the next generation.
Wenyuan Zhao   +3 more
doaj   +1 more source

Turboelectric Distributed Propulsion Protection System Design Trades [PDF]

open access: yesSAE Technical Paper Series, 2014
<div class="section abstract"><div class="htmlview paragraph">The Turboelectric Distributed Propulsion (TeDP) concept uses gas turbine engines as prime movers for generators whose electrical power is used to drive motors and propulsors. For this NASA N3-X study, the motors, generators, and DC transmission lines are superconducting, and the ...
Ross, C.   +5 more
openaire   +2 more sources

Aspects of yaw control design of an aircraft with distributed electric propulsion

open access: yesCEAS Aeronautical Journal, 2022
AbstractDistributed electric propulsion (DEP) offers new options in aircraft design. Besides the optimization of the wing, another area of optimization is the vertical tail plane (VTP) and yaw control. The large number of engines significantly relaxes the one-engine-inoperative (OEI) case during take-off, which is mostly the sizing case for the VTP ...
Vechtel, Dennis, Buch, Jan-Philipp
openaire   +3 more sources

Vibration Characteristics and Power Flow Analyses of a Ship Propulsion Shafting System with General Support and Thrust Loading

open access: yesShock and Vibration, 2020
In this paper, flexural vibration and power flow transmission of a ship propulsion shafting structure are analyzed via energy principle description in conjunction with Rayleigh–Ritz procedure, in which the shafting vibration displacement is constructed ...
Deshui Xu, Jingtao Du, Chuan Tian
doaj   +1 more source

Preliminary Noise Assessment of Aircraft with Distributed Electric Propulsion [PDF]

open access: yes2018 AIAA/CEAS Aeroacoustics Conference, 2018
Electric and hybrid-electric propulsion technologies in aviation are becoming more attractive\ud for aviation stakeholders not only due to the resulting reduction or elimination of the\ud dependency on oil, whose availability and price are uncertain, but also because they are more\ud reliable and efficient than traditional internal combustion engines ...
Synodinos, AP   +2 more
openaire   +1 more source

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