Challenges of future aircraft propulsion: A review of distributed propulsion technology and its potential application for the all electric commercial aircraft
AS Gohardani, G Doulgeris, R Singh - Progress in Aerospace Sciences, 2011 - Elsevier
This paper highlights the role of distributed propulsion technology for future commercial
aircraft. After an initial historical perspective on the conceptual aspects of distributed …
aircraft. After an initial historical perspective on the conceptual aspects of distributed …
A synergistic glance at the prospects of distributed propulsion technology and the electric aircraft concept for future unmanned air vehicles and commercial/military …
AS Gohardani - Progress in Aerospace Sciences, 2013 - Elsevier
Distributed propulsion is one of the revolutionary candidates for future aircraft propulsion. In
this journal article, the potential role of distributed propulsion technology in future aviation is …
this journal article, the potential role of distributed propulsion technology in future aviation is …
Review of propulsion technologies for N+ 3 subsonic vehicle concepts
SW Ashcraft, AS Padron, KA Pascioni, GW Stout Jr… - 2011 - ntrs.nasa.gov
NASA has set aggressive fuel burn, noise, and emission reduction goals for a new
generation (N+ 3) of aircraft targeting concepts that could be viable in the 2035 timeframe …
generation (N+ 3) of aircraft targeting concepts that could be viable in the 2035 timeframe …
Multidisciplinary design optimization of blended-wing-body transport aircraft with distributed propulsion
L Leifsson, A Ko, WH Mason, JA Schetz… - Aerospace Science and …, 2013 - Elsevier
The idea of using distributed propulsion has been suggested with the objective of reducing
aircraft noise. This paper investigates the effects of such a system on aircraft performance …
aircraft noise. This paper investigates the effects of such a system on aircraft performance …
Performance analysis of turbo-electric propulsion system with fuselage boundary layer ingestion
S Samuelsson, T Grönstedt - Aerospace Science and Technology, 2021 - Elsevier
A propulsion system analysis of an aircraft concept featuring a fuselage tail cone integrated
turbo-electrically powered fan is presented. The aircraft has two underwing podded geared …
turbo-electrically powered fan is presented. The aircraft has two underwing podded geared …
[HTML][HTML] A review of novel and non-conventional propulsion integrations for next-generation aircraft
The aim of this review paper is to collect and discuss the most relevant and updated
contributions in the literature regarding studies on new or non-conventional technologies for …
contributions in the literature regarding studies on new or non-conventional technologies for …
[PDF][PDF] 分布式动力系统参数对翼身融合布局无人机气动特性的影响
张阳, 周洲, 王科雷, 范中允 - 西北工业大学学报, 2021 - scholar.archive.org
以耦合分布式动力系统的边界层吸入(BLI) 翼身融合(BWB) 布局无人机为研究对象,
研究了动力系统参数对全机在巡航/起飞条件下的气动影响. 使用动量源方法(MSM) 对NASA …
研究了动力系统参数对全机在巡航/起飞条件下的气动影响. 使用动量源方法(MSM) 对NASA …
Flight mechanics modeling of the PrandtlPlane for conceptual and preliminary design
M Voskuijl, J de Klerk, D van Ginneken - … from a Workshop held at the …, 2012 - Springer
The conceptual and preliminary design of a 300-passenger box-wing aircraft configuration,
designated the PrandtlPlane, is investigated. Currently there are still a number of technical …
designated the PrandtlPlane, is investigated. Currently there are still a number of technical …
Computational analysis of the effects of a boundary layer ingesting propulsion system in transonic flow
V Mantič-Lugo, G Doulgeris… - Proceedings of the …, 2013 - journals.sagepub.com
Continuous requirements for more efficient aircrafts lead to the design and analysis of novel
propulsion configurations, with an example being the boundary layer ingestion. The …
propulsion configurations, with an example being the boundary layer ingestion. The …
Multi-Objective Design of a Distributed Ducted Fan System
J Guo, Z Zhou - Aerospace, 2022 - mdpi.com
The distributed propulsion system applied to the vertical take-off and landing aircraft must
maintain the high performance in both hover and cruise flight. The gap of the power unit has …
maintain the high performance in both hover and cruise flight. The gap of the power unit has …