AEROACOUSTIC DATA FOR HIGH REYNOLDS NUMBER SUPERSONIC AXISYMMETRIC JETS.

被引：0
|
作者：
Seiner, John M. [1 ]
Ponton, Michael K. [1 ]
机构：
[1] NASA, Langley Research Cent,, Hampton, VA, USA, NASA, Langley Research Cent, Hampton, VA, USA
来源：
NASA Technical Memorandum | 1985年
关键词：
D O I：
暂无
中图分类号：
学科分类号：
摘要：
12
引用
收藏
相关论文
共 50 条
  • [31] Computational Aeroacoustic Characteristics of an Airfoil at Higher Reynolds Number
    Sahasranaman, Ashwin
    Senthilkumar, S.
    Balakrishnan, P.
    RENEWABLE ENERGY SOURCES AND TECHNOLOGIES, 2019, 2161
  • [32] Theoretical and experimental study of supersonic oxygen jets. Industrial application in EAF
    Allemand, B
    Bruchet, P
    Champinot, C
    Melen, S
    Porzucek, F
    REVUE DE METALLURGIE-CAHIERS D INFORMATIONS TECHNIQUES, 2001, 98 (06): : 571 - 587
  • [33] CROSSED HOT-WIRE MEASUREMENTS IN LOW TO MODERATE REYNOLDS-NUMBER SUPERSONIC JETS
    SWEARINGEN, JD
    MCLAUGHLIN, DK
    TROUTT, TR
    BULLETIN OF THE AMERICAN PHYSICAL SOCIETY, 1978, 23 (08): : 1016 - 1016
  • [34] ON THE INFLUENCE OF THE NOZZLE EXTERNAL CONFIGURATION ON THE RADIATED SCREECH AND THE DECAY OF SUPERSONIC JETS.
    Carlomagno, Giovanni Maria
    Ianniello, Carmine
    Vigo, Paolo
    Archives of Acoustics, 1981, 6 (02) : 123 - 134
  • [35] Aerodynamic and aeroacoustic performance of a pitching foil with trailing edge serrations at a high Reynolds number
    Ji, Xueyu
    Wang, Li
    Ravi, Sridhar
    Young, John
    Lai, Joseph C. S.
    Tian, Fang-Bao
    THEORETICAL AND COMPUTATIONAL FLUID DYNAMICS, 2024, 38 (06) : 825 - 844
  • [36] A COMPARISON BETWEEN NUMERICAL AND EXPERIMENTAL HIGH REYNOLDS NUMBER SUPERSONIC JETS GENERATED BY MILLIMETER SCALE CONVERGING-DIVERGING NOZZLES
    Conahan, Joseph M.
    Ozdemir, Ozan C.
    Taslim, Mohammad E.
    Muftu, Sinan
    PROCEEDINGS OF THE ASME 2020 INTERNATIONAL MECHANICAL ENGINEERING CONGRESS AND EXPOSITION, IMECE2020, VOL 12, 2020,
  • [37] Numerical study of hydromagnetic axisymmetric peristaltic flow at high Reynolds number and wave number
    A. H. Hamid
    Tariq Javed
    N. Ali
    Biophysical Reviews, 2019, 11 (2) : 139 - 147
  • [38] High Reynolds number thick axisymmetric turbulent boundary layer measurements
    Cipolla, KM
    Keith, WL
    EXPERIMENTS IN FLUIDS, 2003, 35 (05) : 477 - 485
  • [39] Active control of a high reynolds number Mach 0.9 axisymmetric Jet
    Kim, J.-H.
    Kastner, J.
    Samimy, M.
    AIAA Journal, 2009, 47 (01): : 116 - 128
  • [40] On inwardly propagating high-Reynolds-number axisymmetric gravity currents
    Hallworth, M
    Huppert, HE
    Ungarish, M
    JOURNAL OF FLUID MECHANICS, 2003, 494 : 255 - 274
12345