Integration of the Athena Vortex Lattice Aerodynamic Analysis Software into the Multivariate Design Synthesis of Blended Wing Body Aircraft

被引:0
|
作者
Department of Aerospace Engineering, Air Force Institution of Technology, Kaduna, Nigeria [1 ]
机构
来源
| 1600年
关键词
Aerodynamic analysis - Athena vortex lattice - Blended wing body - Blended wing body aircrafts - Design synthesis - Multivariate design - Optimisations - Vortex lattice aerodynamics - Vortex lattices;
D O I
暂无
中图分类号
学科分类号
摘要
18
引用
收藏
相关论文
共 50 条
  • [31] Propulsion and Flight Controls Integration for a Blended-Wing-Body Transport Aircraft
    Rahman, Naveed U.
    Whidborne, James F.
    JOURNAL OF AIRCRAFT, 2010, 47 (03): : 895 - 903
  • [32] Aerodynamic Design, Analysis and Validation of a Small Blended-Wing-Body Unmanned Aerial Vehicle
    Wang, Kelei
    Zhou, Zhou
    AEROSPACE, 2022, 9 (01)
  • [33] Design and Comparison of Hydrogen SOFC/GT in Blended Wing Body Aircraft
    Chung, Vanessa
    Alsamri, Khaled
    Huynh, Jacqueline
    Brouwer, Jack
    AIAA AVIATION FORUM AND ASCEND 2024, 2024,
  • [34] Design of Krueger flap for civil aircraft with blended-wing-body
    Zhang M.
    Chen Z.
    Mao J.
    Wang G.
    Tan Z.
    Wang L.
    Zhang B.
    Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2019, 40 (09):
  • [35] Intake and exhaust effect on aerodynamic characteristics of blended wing body civil aircraft with podded engines
    Gu W.
    Chen Y.
    Xin Z.
    Chen Z.
    Zhang B.
    Hangkong Dongli Xuebao/Journal of Aerospace Power, 2019, 34 (06): : 1297 - 1310
  • [36] Research progress and prospect for conceptual and aerodynamic technology of blended-wing-body civil aircraft
    Wang G.
    Zhang B.
    Zhang M.
    Sang W.
    Yuan C.
    Li D.
    Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2019, 40 (09):
  • [37] Airfoil Design Optimization of Blended Wing Body for Various Aerodynamic and Stealth Stations
    Zhang, Wei
    Zhou, Lin
    Zhao, Ke
    Zhang, Ruibin
    Gao, Zhenghong
    Shu, Bowen
    AEROSPACE, 2024, 11 (07)
  • [38] Aerodynamic Evaluation of UiTM's Blended Wing Body Unmanned Aerial Vehicle at Different Elevon Configurations using Vortex Lattice Method
    Osman, Azraai
    Hamid, Ahmad Hussein Abdul
    Yusof, Muhammad Fida'iy Najmie Mohamed
    Nasir, Rizal Effendy Mohd
    JOURNAL OF AERONAUTICS ASTRONAUTICS AND AVIATION, 2024, 56 (01): : 419 - 437
  • [39] Design optimization for the entire aircraft structure of civil aircraft with blended-wing-body layout
    Zhang, Yongjie
    Zhou, Jingpiao
    Shi, Lei
    Cui, Bo
    STRUCTURAL AND MULTIDISCIPLINARY OPTIMIZATION, 2024, 67 (06)
  • [40] Multidisciplinary design optimization of aircraft wing using commercial software integration
    Benaouali, Abdelkader
    Kachel, Stanislaw
    AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 92 : 766 - 776