Application of Multipole Decomposition for Sonic Boom Propagation Problems

被引:0
作者
Kornyakov, A. A. [1 ]
Soudakova, V. G. [1 ]
Shcheglova, A. S. [1 ]
机构
[1] Zhukovsky Cent Aerohydrodynam Inst, Zhukovskii 140181, Russia
关键词
sonic boom; multipole decomposition; supersonic transport; near field; far field;
D O I
10.3103/S0025654423080113
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
In the present, work a modification of the multipole decomposition method is developed, which makes it possible to relate the overpressure distribution in the near-field of a supersonic transport (SST) with a far-field distribution, which is needed for the solution of sonic boom propagation problem from an SST. A generalization of the method for solving the integral equations arising from multipole decomposition is performed. An algorithm for multipole correction of near-field overpressure signatures obtained in numerical simulations has been developed and tested.
引用
收藏
页码:2933 / 2943
页数:11
相关论文
共 16 条
  • [1] [Anonymous], 1972, D6832 NASA
  • [2] Re-entry vehicle sonic boom issue: Modelling and calculation results in windy atmosphere based on the augmented Burgers equation
    Chernyshev, S. L.
    Gorbovskoy, V. S.
    Kazhan, A., V
    Korunov, A. O.
    [J]. ACTA ASTRONAUTICA, 2022, 194 : 450 - 460
  • [3] Chernyshev S. L., 2011, Sound Impact
  • [4] Theoretical Modeling of Two-Body Interaction in Supersonic Flow
    Fedorov, Alexander V.
    Soudakov, Vitaly G.
    Malmuth, Norman D.
    [J]. AIAA JOURNAL, 2010, 48 (02) : 258 - 266
  • [5] REDUCTION OF SONIC BOOM BY AZIMUTHAL REDISTRIBUTION OF OVERPRESSURE
    GEORGE, AR
    [J]. AIAA JOURNAL, 1969, 7 (02) : 291 - &
  • [6] Extension of Multipole Analysis to Laterally Asymmetric Flowfield Around Supersonic Flight Vehicle
    Kanamori, Masashi
    Makino, Yoshikazu
    Ishikawa, Hiroaki
    [J]. JOURNAL OF AIRCRAFT, 2019, 56 (01): : 191 - 204
  • [7] GEOMETRICAL ACOUSTICS .1. THE THEORY OF WEAK SHOCK WAVES
    KELLER, JB
    [J]. JOURNAL OF APPLIED PHYSICS, 1954, 25 (08) : 938 - 947
  • [8] Landau LD., 1945, J PHYS-USSR, V9, P496
  • [9] Maglieri D. J., 2014, NASASP2014622
  • [10] Page J. A., 1991, 9th Applied Aerodynamics Conference, DOI [10.2514/6.1991-3275, DOI 10.2514/6.1991-3275]