Generic design methodology for vertical takeoff and landing aircraft with hybrid-electric propulsion
This paper proposes a conceptual methodology for designing vertical takeoff and landing
aircraft with a hybrid-electric propulsion system as an alternative to facilitate intercity …
aircraft with a hybrid-electric propulsion system as an alternative to facilitate intercity …
Effects of design parameters on coaxial rotorcraft with propellers on wing tips
RECENTLY, an additional thrust source or lifting device is used in a compound rotorcraft for
improving cruise performance and facilitating unique flight capabilities such as vertical …
improving cruise performance and facilitating unique flight capabilities such as vertical …
[PDF][PDF] A comparison study of rotorcraft with hybrid electric propulsion system
D Lee, S Kang, K Yee - … of the 45th European Rotorcraft Forum …, 2018 - dspace-erf.nlr.nl
ABSTRACT Hybrid Electric Propulsion System (HEPS) is being developed as a novel
propulsion system not only for the reduction of carbon emission but also for significant …
propulsion system not only for the reduction of carbon emission but also for significant …
Physics-Based Airframe Design Approach Expanded from the Conceptual Design of Coaxial Rotorcraft
C Ahn, WS Cha, SH Park, BU Im, TY Chun… - International Journal of …, 2024 - Springer
Unconventional configurations are required to satisfy the existing niche in conventional
rotorcraft owing to the increasing demands for high-speed rotorcraft operations. Thus, this …
rotorcraft owing to the increasing demands for high-speed rotorcraft operations. Thus, this …
Generic System Design Methodology for eVTOL Aircraft using Enhanced Electric Propulsion Modeling
이동욱 - 2023 - s-space.snu.ac.kr
In recent years, various technological advances in electrification, automation, and vertical
takeoff and landing (VTOL) have matured enough to enable innovation in urban aviation …
takeoff and landing (VTOL) have matured enough to enable innovation in urban aviation …
[HTML][HTML] Математическая модель для расчета летно-технических характеристик электрических винтокрылых летательных аппаратов для целей городской …
МИ Мясников, ИР Ильин - Научный вестник Московского …, 2023 - cyberleninka.ru
В настоящей работе приводится описание математической модели, разработанной
для расчета летнотехнических характеристик (ЛТХ) наиболее популярных в настоящее …
для расчета летнотехнических характеристик (ЛТХ) наиболее популярных в настоящее …
Improved Probabilistic Design Process for Advanced Air Mobility with Technology Portfolio Assessment
임대진 - 2023 - s-space.snu.ac.kr
Within the last several decades, breakthroughs in multiple disciplines of aircraft technology
and design have paved the way to the advent of a novel aircraft system that is collectively …
and design have paved the way to the advent of a novel aircraft system that is collectively …
[引用][C] 하이브리드전기추진시스템을이용하는복합형회전익기개념설계연구
이동욱, 강세권, 이관중 - 한국항공우주학회학술발표회초록집, 2019 - dbpia.co.kr
하이브리드 전기추진시스템 (Hybrid Electric Propulsion System, HEPS) 은 기존의 내연기관
시스템과 전기추진장치들이 결합된 추진시스템으로, 배터리와 탄화수소 연료를 …
시스템과 전기추진장치들이 결합된 추진시스템으로, 배터리와 탄화수소 연료를 …