Segui
Donguk Lee
Titolo
Citata da
Citata da
Anno
Generic design methodology for vertical takeoff and landing aircraft with hybrid-electric propulsion
D Lee, D Lim, K Yee
Journal of Aircraft 59 (2), 278-292, 2022
482022
A refined sizing method of fuel cell-battery hybrid system for eVTOL aircraft
J Park, D Lee, D Lim, K Yee
Applied Energy 328, 120160, 2022
322022
A COMPARISION STUDY OF ROTORCRAFT WITH HYBRID ELECTRIC PROPULSION SYSTEM
D Lee, S Kang, K Yee
45th European Rotorcraft Forum, 2019
112019
Development of Fuel Cell/Battery Hybrid System Sizing Methodology for eVTOL Aircraft
J Park, D Lee, K Yee
AIAA AVIATION 2022 Forum, 3514, 2022
92022
Development of a conceptual design tool for various compound helicopters
D Lee, S Jeong, K Yee
82018
ADVANCED ANALYSIS METHOD OF ELECTRIC PROPULSION SYSTEM FOR UAM VEHICLES
D Lee, K Yee
47th European Rotorcraft Forum, 2021
62021
Sizing Methodology and Performance Assessment of Hybrid Electric Propulsion Aircraft
S Kang, D Lee, S Jeong, K Yee
7th Asian Rotorcraft Forum, 2018
62018
Development of Conceptual Design Methodology and Initial Sizing for Tip-Jet Gyroplane
D Lee, D Lim, K Yee
Journal of the Korean Society for Aeronautical & Space Sciences 46 (6), 452-463, 2018
42018
Novel Electric Propulsion System Analysis Method for Electric Vertical Takeoff and Landing Aircraft Conceptual Design
D Lee, K Yee
Journal of Aircraft 61 (2), 375-391, 2024
32024
Development of Conceptual Design Method of Compound Rotorcraft using Lift Fan
S Jeong, D Lee, K Yee
7th Asian Rotorcraft Forum, 2018
32018
Technology Portfolio Assessment with Uncertainty Consideration for Advanced Air Mobility
D Lim, D Lee, K Yee
AIAA AVIATION 2022 Forum, 3660, 2022
12022
도심 항공 모빌리티를 위한 하이브리드 전기추진시스템 기반 수직이착륙기 개념 설계
이동욱, 이관중
한국항공우주학회 학술발표회 초록집, 269-270, 2020
12020
Tip jet 구동 방식을 이용한 자이로플레인 개념설계 기법 개발
이동욱, 김형석, 이관중
한국항공우주학회 학술발표회 초록집, 515-516, 2017
12017
Improved Conceptual Design of eVTOL Aircraft: Considering Rotor–Rotor Interactional Effects
H Kim, J Lee, D Lee, K Yee
International Journal of Aeronautical and Space Sciences, 1-20, 2025
2025
Improved Turboelectric System Modeling for Conceptual Design of Vertical Take Off and Landing Aircraft< TITLE lang=""> 수직이착륙기 개념설계를 위한 개선된 터보일렉트릭 시스템 …
J Cho, D Lee, J Park, T Jeong, K Yee
Journal of the Korean Society for Aeronautical & Space Sciences 53 (1), 63-76, 2025
2025
수직이착륙기 개념설계를 위한 개선된 터보일렉트릭 시스템 모델링
조재현, 이동욱, 박준휘, 정태민, 이관중
한국항공우주학회지 53 (1), 63-76, 2025
2025
Correction: Novel Electric Propulsion System Analysis Method for eVTOL Aircraft Conceptual Design
D Lee, K Yee
Journal of Aircraft 61 (6), 1-2, 2024
2024
개선된 제너레이터 시스템 모델링을 이용한 터보일렉트릭 추진시스템 기반 수직이착륙 미래 항공 모빌리티 항공기 개념설계
조재현, 이동욱, 박준휘, 정태민, 이관중
한국항공우주학회 학술발표회 초록집, 416-417, 2024
2024
화성 탐사 수직이착륙 비행체 개념설계 연구
이동욱, 권순명, 박성중, 이관중
한국항공우주학회 학술발표회 초록집, 268-269, 2023
2023
화성 탐사 비행체-로버 협업 시스템을 위한 ConOps 및 비행체 형상 후보군 제시
박성중, 이동욱, 권순명, 이관중
한국항공우주학회 학술발표회 초록집, 266-267, 2023
2023
Il sistema al momento non può eseguire l'operazione. Riprova più tardi.
Articoli 1–20