Validity of the Concept of the Unit Grid Fin by 3-D Calculation of Supersonic Grid Fin Flows

被引：0
|
作者：
Lee, Hyeong Jin [1 ]
Ko, Sang Ho [2 ]
Kang, Tae Gon [2 ]
Lee, Yeol [2 ]
机构：
[1] Korea Aerosp Univ, Grad Sch, Dept Aerosp & Mech Engn, Goyang, South Korea
[2] Korea Aerosp Univ, Sch Aerosp & Mech Engn, Goyang, South Korea
来源：
JOURNAL OF THE KOREAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES | 2021年 / 49卷 / 08期
关键词：
Supersonic; Grid Fin; Unit Grid Fin; Shock Wave; MISSILE;
D O I：
10.5139/JKSAS.2021.49.8.609
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
Three-dimensional numerical study was carried out to evaluate the aerodynamic characteristics of the supersonic grid fins installed on SpaceX Falcon 9. The present three-dimensional flow results were compared to the results by the concept of the unit grid fin previously introduced for more efficient and simpler flow calculations, and the validity of the approach of the unit grid fin were evaluated. The aerodynamic characteristics in supersonic flights Mach 2.8 of SpaceX Falcon 9 with various angle of attacks were also obtained.
引用
收藏
页码：609 / 615
页数：7
相关论文
共 50 条
  • [1] Calculation and analysis of grid fin configurations
    Tong, ZL
    Lu, ZR
    Shen, XL
    STRENGTHENING COOPERATION IN THE 21ST CENTURY, 1996, 91 : 1017 - 1023
  • [2] Calculation and analysis of grid fin configurations
    Lu, Zhongrong
    Shen, Xialing
    Tong, Zili
    Zhao, Heshu
    Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics, 1996, 22 (05): : 575 - 580
  • [3] Aerodynamic analysis of grid-fin configurations at supersonic speeds
    Theerthamalai, P.
    Nagarathinam, M.
    JOURNAL OF SPACECRAFT AND ROCKETS, 2006, 43 (04) : 750 - 756
  • [4] GRID GENERATION IN SPACE AND CALCULATION FOR 3-D TURBULENT FLOW
    Zheng Bong-min
    Chao Ming-deng
    Journal of Hydrodynamics(SerB)., 1991, (01) : 66 - 71
  • [5] CALCULATION PROCEDURE FOR 3-D LAMINAR FLOWS IN COMPLEX GEOMETRIES USING A NONSTAGGERED NONORTHOGONAL GRID SYSTEM
    COELHO, P
    PEREIRA, JCF
    APPLIED MATHEMATICAL MODELLING, 1993, 17 (11) : 562 - 576
  • [6] Optimization of a 3-D thermally asymmetric rectangular fin
    Hyuag Suk Kang
    KSME International Journal, 2001, 15 : 1541 - 1547
  • [7] Stacked 3-D Fin-CMOS technology
    Wu, XS
    Chan, PCH
    Zhang, SD
    Feng, CG
    Chan, MS
    IEEE ELECTRON DEVICE LETTERS, 2005, 26 (06) : 416 - 418
  • [8] Optimization of a 3-D thermally asymmetric rectangular fin
    Kang, HS
    KSME INTERNATIONAL JOURNAL, 2001, 15 (11): : 1541 - 1547
  • [9] A New Algorithm for Shock Sensor Calculation at Supersonic Speeds on a 3D-Unstructured Grid
    Tahmasbi, Vahid
    Karimian, Seyed Mohammad Hossein
    JOURNAL OF AEROSPACE TECHNOLOGY AND MANAGEMENT, 2016, 8 (04) : 441 - 450
  • [10] Characteristics of the Supersonic Flows Over 3-D Bump
    James, Jintu K.
    Kim, Heuy Dong
    RECENT ASIAN RESEARCH ON THERMAL AND FLUID SCIENCES, AJWTF7 2018, 2020, : 421 - 431
12345