8
views
0
recommends
+1 Recommend
1 collections
    0
    shares

      To publish with AIAA, please click here

      • Record: found
      • Abstract: found
      • Article: found

      Temperature Effects on Convection Speed and Steepened Waves of Temporally Developing Supersonic Jets

      research-article
      * ,
      AIAA Journal
      American Institute of Aeronautics and Astronautics

      Read this article at

      ScienceOpenPublisher
      Bookmark
          There is no author summary for this article yet. Authors can add summaries to their articles on ScienceOpen to make them more accessible to a non-specialist audience.

          Abstract

          Temperature effects on the convection speed of large-scale structures in supersonic temporally developing jets and on the steepened aspect of the acoustic waves generated by these structures are investigated. For that, one isothermal jet at Mach 2 and four others at static temperatures equal to two or four times that of the ambient medium are simulated at either the same exit velocity or Mach number as the isothermal jet. For all temporally developing jets, steepened acoustic waves are emitted in the near field, leading to significant values of the pressure skewness and kurtosis factors. Using conditional averages, their formation is directly linked to the supersonic motion of large-scale structures at a convection speed whose ratio with the jet velocity is shown to decrease with temperature. At a higher temperature, this leads to the generation of less skewed acoustic waves for a constant jet velocity. For a constant Mach number, however, this decrease is compensated by the rise of the jet speed, leading to steeper acoustic waves at a higher temperature. Therefore, the modification of the steepened aspect of near-field acoustic waves appears to be related to the change in the convection speed in both cases.

          Related collections

          Most cited references56

          • Record: found
          • Abstract: not found
          • Article: not found

          An experimental study of jet noise part I: Turbulent mixing noise

          H.K. Tanna (1977)
            Bookmark
            • Record: found
            • Abstract: not found
            • Article: not found

            RADIATION AND OUTFLOW BOUNDARY CONDITIONS FOR DIRECT COMPUTATION OF ACOUSTIC AND FLOW DISTURBANCES IN A NONUNIFORM MEAN FLOW

              Bookmark
              • Record: found
              • Abstract: not found
              • Article: not found

              A shock-capturing methodology based on adaptative spatial filtering for high-order non-linear computations

                Bookmark

                Author and article information

                Journal
                aiaaj
                AIAA Journal
                AIAA Journal
                American Institute of Aeronautics and Astronautics
                1533-385X
                27 December 2019
                March 2020
                : 58
                : 3
                : 1227-1239
                Affiliations
                École Centrale de Lyon , F-69134 Ecully, France
                Author notes
                [*]

                Ph.D., CNES Post-Doctoral Fellow, Univ Lyon, École Centrale de Lyon, INSA Lyon, Université Claude Bernard Lyon I, CNRS, Laboratoire de Mécanique des Fluides et d’Acoustique, UMR 5509; pierre.pineau@ 123456doctorant.ec-lyon.fr .

                [†]

                CNRS Research Scientist, Univ Lyon, École Centrale de Lyon, INSA Lyon, Université Claude Bernard Lyon I, CNRS, Laboratoire de Mécanique des Fluides et d’Acoustique, UMR 5509. Senior Member AIAA.

                Article
                J058589 J058589
                10.2514/1.J058589
                bc577e9d-03b8-4fd5-8a54-7a98fb4859dc
                Copyright © 2019 by Pierre Pineau. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the eISSN 1533-385X to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp.
                History
                : 23 April 2019
                : 2 October 2019
                : 15 November 2019
                Page count
                Figures: 20, Tables: 1
                Categories
                Regular Articles

                Engineering,Physics,Mechanical engineering,Space Physics
                Engineering, Physics, Mechanical engineering, Space Physics

                Comments

                Comment on this article