Blended Wing-Body Unmanned Aerial Transport Aircraft: A conceptual design

被引:0
|
作者
Nasir, Rizal Effendy Mohd [1 ]
Mohamad, Firdaus [1 ]
Hamid, Ahmad Hussein Abdul [1 ]
Noh, Mohd Hafiz Mohd [1 ]
机构
[1] Univ Teknol MARA, Coll Engn, Flight Technol & Test Res Grp, Shah Alam 40450, Selangor, Malaysia
关键词
Air Transport; Blended Wing -Body; Unmanned Aerial Vehicle;
D O I
暂无
中图分类号
X [环境科学、安全科学];
学科分类号
08 ; 0830 ;
摘要
UAVs have advantages for tasks like aerial surveillance, agriculture, and transportation because of their low operating costs and the ability to automate the work. This paper introduces a conceptual design of a parcel transport UAV called Baseline-X BWB that carries two kilogrammes of payload for intercity transport. The scope of discussion is limited to aerodynamic estimation, flight performance, and monetary cost. This UAV prototype has a longer battery charge range, a larger and heavier payload capacity, and a lower operating cost-per-mile and fleet cost per route than conventional designs of the same size, making it feasible and profitable for operators.
引用
收藏
页码:601 / 610
页数:10
相关论文
共 50 条
  • [1] Blended Wing-Body Unmanned Aerial Transport Aircraft: A conceptual design
    Nasir, Rizal Effendy Mohd
    Mohamad, Firdaus
    Hamid, Ahmad Hussein Abdul
    Noh, Mohd Hafiz Mohd
    ENVIRONMENT-BEHAVIOUR PROCEEDINGS JOURNAL, 2022, 7 : 601 - 610
  • [2] Flight Performance Analysis of a Blended Wing-Body Unmanned Aerial Transport Vehicle
    Shuairi, Muhammad Danial Mohamad
    Nasir, Rizal Effendy Mohd
    Romli, Fairuz Izzuddin
    JOURNAL OF AERONAUTICS ASTRONAUTICS AND AVIATION, 2024, 56 (01): : 243 - 256
  • [3] Conceptual design and analysis of blended-wing-body aircraft
    van Dommelen, Jorrit
    Vos, Roelof
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2014, 228 (13) : 2452 - 2474
  • [4] CONCEPTUAL DESIGN OF A 200 PASSENGERS BLENDED WING BODY AIRCRAFT
    Ammar, Sami
    Trepanier, Jean-Yves
    PROCEEDINGS OF THE ASME INTERNATIONAL MECHANICAL ENGINEERING CONGRESS AND EXPOSITION, 2014, VOL 1, 2015,
  • [5] Effect of geometric variations on the wing rock of blended wing-body aircraft
    Siddiqui, Waseeq
    Maqsood, Adnan
    Salamat, Shuaib
    Xu, Hongyi
    Dan, Xie
    INTERNATIONAL JOURNAL OF NON-LINEAR MECHANICS, 2025, 168
  • [6] Aerodynamic Design Optimization of Wing-body/Blended-wing-body Configuration
    Li, Yun
    Yuan, Xiangjiang
    AEIT 2012: 2012 2ND INTERNATIONAL CONFERENCE ON AEROSPACE ENGINEERING AND INFORMATION TECHNOLOGY, VOL 2, 2012, : 154 - 162
  • [7] Structural mass prediction in conceptual design of blended-wing-body aircraft
    Wensheng ZHU
    Zhouwei FAN
    Xiongqing YU
    Chinese Journal of Aeronautics, 2019, 32 (11) : 2455 - 2465
  • [8] Structural mass prediction in conceptual design of blended-wing-body aircraft
    Wensheng ZHU
    Zhouwei FAN
    Xiongqing YU
    Chinese Journal of Aeronautics , 2019, (11) : 2455 - 2465
  • [9] Structural mass prediction in conceptual design of blended-wing-body aircraft
    Zhu, Wensheng
    Fan, Zhouwei
    Yu, Xiongqing
    CHINESE JOURNAL OF AERONAUTICS, 2019, 32 (11) : 2455 - 2465
  • [10] Wing design for blended-wing-body aircraft
    Yazik, M. H. Mat
    Sultan, M. T. H.
    Hamdan, A.
    PROCEEDINGS OF MECHANICAL ENGINEERING RESEARCH DAY 2017 (MERD), 2017, : 142 - 143