Skip to main content
Erschienen in: Journal of Visualization 6/2021

26.07.2021 | Regular Paper

Comparison of three-dimensional density distribution of numerical and experimental analysis for twin jets

verfasst von: Chungil Lee, Yuta Ozawa, Takanori Haga, Taku Nonomura, Keisuke Asai

Erschienen in: Journal of Visualization | Ausgabe 6/2021

Einloggen

Aktivieren Sie unsere intelligente Suche, um passende Fachinhalte oder Patente zu finden.

search-config
loading …

Abstract

Three-dimensional density fields of the twin jets were numerically and experimentally investigated. The present study focused on the comparison of the density distribution for the twin jets. The results obtained by the computational fluid dynamics (CFD) and three-dimensional background-oriented schlieren (3D-BOS) indicate that the periodic density fluctuation appears in the potential core each nozzle, and the flow structure of the twin jets is quite similar. The distribution of the normalized density value at the nozzle centerline agrees well with CFD and 3D-BOS. The density value of the shear layer between the nozzles increases as the interaction of the twin jets occurs. The trend of increasing and decreasing the interference between the nozzles was almost the same as each other. On the other hand, the position where the interaction of the twin jets starts and the growth rate of interaction were different. This is probably due to the effect of the laminar-to-turbulent transition occurred in the results of CFD. This result indicates that the laminar-to-turbulent transition can be estimated from the velocity fields obtained by CFD and particle image velocimetry (PIV).

Graphic Abstract

Sie haben noch keine Lizenz? Dann Informieren Sie sich jetzt über unsere Produkte:

Springer Professional "Wirtschaft+Technik"

Online-Abonnement

Mit Springer Professional "Wirtschaft+Technik" erhalten Sie Zugriff auf:

  • über 102.000 Bücher
  • über 537 Zeitschriften

aus folgenden Fachgebieten:

  • Automobil + Motoren
  • Bauwesen + Immobilien
  • Business IT + Informatik
  • Elektrotechnik + Elektronik
  • Energie + Nachhaltigkeit
  • Finance + Banking
  • Management + Führung
  • Marketing + Vertrieb
  • Maschinenbau + Werkstoffe
  • Versicherung + Risiko

Jetzt Wissensvorsprung sichern!

Springer Professional "Wirtschaft"

Online-Abonnement

Mit Springer Professional "Wirtschaft" erhalten Sie Zugriff auf:

  • über 67.000 Bücher
  • über 340 Zeitschriften

aus folgenden Fachgebieten:

  • Bauwesen + Immobilien
  • Business IT + Informatik
  • Finance + Banking
  • Management + Führung
  • Marketing + Vertrieb
  • Versicherung + Risiko




Jetzt Wissensvorsprung sichern!

Springer Professional "Technik"

Online-Abonnement

Mit Springer Professional "Technik" erhalten Sie Zugriff auf:

  • über 67.000 Bücher
  • über 390 Zeitschriften

aus folgenden Fachgebieten:

  • Automobil + Motoren
  • Bauwesen + Immobilien
  • Business IT + Informatik
  • Elektrotechnik + Elektronik
  • Energie + Nachhaltigkeit
  • Maschinenbau + Werkstoffe




 

Jetzt Wissensvorsprung sichern!

Anhänge
Nur mit Berechtigung zugänglich
Literatur
Zurück zum Zitat Abe Y, Haga T, Nonomura T, Fujii K (2015) On the freestream preservation of high-order conservative flux-reconstruction schemes. J Comput Phys 281:28–54MathSciNetCrossRef Abe Y, Haga T, Nonomura T, Fujii K (2015) On the freestream preservation of high-order conservative flux-reconstruction schemes. J Comput Phys 281:28–54MathSciNetCrossRef
Zurück zum Zitat Abe Y, Morinaka I, Haga T, Nonomura T, Shibata H, Miyaji K (2018) Stable, non-dissipative, and conservative flux-reconstruction schemes in split forms. J Comput Phys 353:193–227MathSciNetCrossRef Abe Y, Morinaka I, Haga T, Nonomura T, Shibata H, Miyaji K (2018) Stable, non-dissipative, and conservative flux-reconstruction schemes in split forms. J Comput Phys 353:193–227MathSciNetCrossRef
Zurück zum Zitat Amiet R (1978) Refraction of sound by a shear layer. J Sound Vib 58(4):467–482CrossRef Amiet R (1978) Refraction of sound by a shear layer. J Sound Vib 58(4):467–482CrossRef
Zurück zum Zitat Bauknecht A, Ewers B, Wolf C, Leopold F, Yin J, Raffel M (2015) Three-dimensional reconstruction of helicopter blade-tip vortices using a multi-camera bos system. Exp Fluids 56(1):1–13CrossRef Bauknecht A, Ewers B, Wolf C, Leopold F, Yin J, Raffel M (2015) Three-dimensional reconstruction of helicopter blade-tip vortices using a multi-camera bos system. Exp Fluids 56(1):1–13CrossRef
Zurück zum Zitat Borchers I, Goethert B (1977) An experimental study of the noise radiation of interfering free jets. In: 4th aeroacoustics conference, p 1285 Borchers I, Goethert B (1977) An experimental study of the noise radiation of interfering free jets. In: 4th aeroacoustics conference, p 1285
Zurück zum Zitat Bozak R, Henderson B (2011) Aeroacoustic experiments with twin jets. In: 17th AIAA/CEAS aeroacoustics conference (32nd AIAA aeroacoustics conference), p 2790 Bozak R, Henderson B (2011) Aeroacoustic experiments with twin jets. In: 17th AIAA/CEAS aeroacoustics conference (32nd AIAA aeroacoustics conference), p 2790
Zurück zum Zitat Freund JB (1997) Proposed inflow/outflow boundary condition for direct computation of aerodynamic sound. AIAA J 35(4):740–742CrossRef Freund JB (1997) Proposed inflow/outflow boundary condition for direct computation of aerodynamic sound. AIAA J 35(4):740–742CrossRef
Zurück zum Zitat Goldhahn E, Seume J (2007) The background oriented schlieren technique: sensitivity, accuracy, resolution and application to a three-dimensional density field. Exp Fluids 43(2–3):241–249CrossRef Goldhahn E, Seume J (2007) The background oriented schlieren technique: sensitivity, accuracy, resolution and application to a three-dimensional density field. Exp Fluids 43(2–3):241–249CrossRef
Zurück zum Zitat Greatrex F, Brown D (1958) Progress in jet engine noise reduction. In: The first international council of the aeronautical sciences, pp 364–392 Greatrex F, Brown D (1958) Progress in jet engine noise reduction. In: The first international council of the aeronautical sciences, pp 364–392
Zurück zum Zitat Haga T, Kawai S (2019) On a robust and accurate localized artificial diffusivity scheme for the high-order flux-reconstruction method. J Comput Phys 376:534–563MathSciNetCrossRef Haga T, Kawai S (2019) On a robust and accurate localized artificial diffusivity scheme for the high-order flux-reconstruction method. J Comput Phys 376:534–563MathSciNetCrossRef
Zurück zum Zitat Hansen PC (1999) The l-curve and its use in the numerical treatment of inverse problems Hansen PC (1999) The l-curve and its use in the numerical treatment of inverse problems
Zurück zum Zitat Hartmann U, Adamczuk R, Seume J (2015) Tomographic background oriented schlieren applications for turbomachinery. In: 53rd AIAA aerospace sciences meeting, p 1690 Hartmann U, Adamczuk R, Seume J (2015) Tomographic background oriented schlieren applications for turbomachinery. In: 53rd AIAA aerospace sciences meeting, p 1690
Zurück zum Zitat Hirose Y, Ishikawa K, Ishimoto Y, Nagashima T, Ota M, Udagawa S, Inage T, Kiritani H, Fujita K, Fujita K et al (2019) The quantitative density measurement of unsteady flow around the projectile. J Flow Control Meas Visual 7(02):111CrossRef Hirose Y, Ishikawa K, Ishimoto Y, Nagashima T, Ota M, Udagawa S, Inage T, Kiritani H, Fujita K, Fujita K et al (2019) The quantitative density measurement of unsteady flow around the projectile. J Flow Control Meas Visual 7(02):111CrossRef
Zurück zum Zitat Huynh HT (2007) A flux reconstruction approach to high-order schemes including discontinuous Galerkin methods. In: 18th AIAA computational fluid dynamics conference, p 4079 Huynh HT (2007) A flux reconstruction approach to high-order schemes including discontinuous Galerkin methods. In: 18th AIAA computational fluid dynamics conference, p 4079
Zurück zum Zitat Jarrin N, Benhamadouche S, Laurence D, Prosser R (2006) A synthetic-eddy-method for generating inflow conditions for large-eddy simulations. Int J Heat Fluid Flow 27(4):585–593CrossRef Jarrin N, Benhamadouche S, Laurence D, Prosser R (2006) A synthetic-eddy-method for generating inflow conditions for large-eddy simulations. Int J Heat Fluid Flow 27(4):585–593CrossRef
Zurück zum Zitat Kantola R (1981) Acoustic properties of heated twin jets. J Sound Vib 79(1):79–106CrossRef Kantola R (1981) Acoustic properties of heated twin jets. J Sound Vib 79(1):79–106CrossRef
Zurück zum Zitat Knast T, Bell G, Wong M, Leb CM, Soria J, Honnery DR, Edgington-Mitchell D (2018) Coupling modes of an underexpanded twin axisymmetric jet. AIAA J 56(9):3524–3535CrossRef Knast T, Bell G, Wong M, Leb CM, Soria J, Honnery DR, Edgington-Mitchell D (2018) Coupling modes of an underexpanded twin axisymmetric jet. AIAA J 56(9):3524–3535CrossRef
Zurück zum Zitat Nicolas F, Todoroff V, Plyer A, Le Besnerais G, Donjat D, Micheli F, Champagnat F, Cornic P, Le Sant Y (2016) A direct approach for instantaneous 3d density field reconstruction from background-oriented schlieren (bos) measurements. Exp Fluids 57(1):13CrossRef Nicolas F, Todoroff V, Plyer A, Le Besnerais G, Donjat D, Micheli F, Champagnat F, Cornic P, Le Sant Y (2016) A direct approach for instantaneous 3d density field reconstruction from background-oriented schlieren (bos) measurements. Exp Fluids 57(1):13CrossRef
Zurück zum Zitat Nonomura T, Nakano H, Ozawa Y, Terakado D, Yamamoto M, Fujii K, Oyama A (2019) Large eddy simulation of acoustic waves generated from a hot supersonic jet. Shock Waves 29:1133–1154CrossRef Nonomura T, Nakano H, Ozawa Y, Terakado D, Yamamoto M, Fujii K, Oyama A (2019) Large eddy simulation of acoustic waves generated from a hot supersonic jet. Shock Waves 29:1133–1154CrossRef
Zurück zum Zitat Nonomura T, Abe Y, Ozawa Y, Fujii K (2021) Computational study on aeroacoustic fields of a transitional supersonic jet. J Am Soc Acoust 149:4484–4502CrossRef Nonomura T, Abe Y, Ozawa Y, Fujii K (2021) Computational study on aeroacoustic fields of a transitional supersonic jet. J Am Soc Acoust 149:4484–4502CrossRef
Zurück zum Zitat Ota M, Hamada K, Kato H, Maeno K (2011) Computed-tomographic density measurement of supersonic flow field by colored-grid background oriented schlieren (cgbos) technique. Meas Sci Technol 22(10):104011CrossRef Ota M, Hamada K, Kato H, Maeno K (2011) Computed-tomographic density measurement of supersonic flow field by colored-grid background oriented schlieren (cgbos) technique. Meas Sci Technol 22(10):104011CrossRef
Zurück zum Zitat Ota M, Kurihara K, Aki K, Miwa Y, Inage T, Maeno K (2015) Quantitative density measurement of the lateral jet/cross-flow interaction field by colored-grid background oriented schlieren (cgbos) technique. J Visual 18(3):543–552CrossRef Ota M, Kurihara K, Aki K, Miwa Y, Inage T, Maeno K (2015) Quantitative density measurement of the lateral jet/cross-flow interaction field by colored-grid background oriented schlieren (cgbos) technique. J Visual 18(3):543–552CrossRef
Zurück zum Zitat Ozawa Y (2020) Aeroacoustic fields of multiple ideally expanded supersonioc jets of mach number of 2.0. Ph. D. Dissertation, Tohoku University, Japan Ozawa Y (2020) Aeroacoustic fields of multiple ideally expanded supersonioc jets of mach number of 2.0. Ph. D. Dissertation, Tohoku University, Japan
Zurück zum Zitat Ozawa Y, Ibuki T, Nonomura T, Suzuki K, Komuro A, Ando A, Asai K (2020a) Single-pixel resolution velocity/convection velocity field of a supersonic jet measured by particle/schlieren image velocimetry. Exp Fluids 61(6):129CrossRef Ozawa Y, Ibuki T, Nonomura T, Suzuki K, Komuro A, Ando A, Asai K (2020a) Single-pixel resolution velocity/convection velocity field of a supersonic jet measured by particle/schlieren image velocimetry. Exp Fluids 61(6):129CrossRef
Zurück zum Zitat Ozawa Y, Nonomura T, Oyama A, Asai K (2020b) Effect of the Reynolds number on the aeroacoustic fields of a transitional supersonic jet. Phys Fluids 32(4):046108CrossRef Ozawa Y, Nonomura T, Oyama A, Asai K (2020b) Effect of the Reynolds number on the aeroacoustic fields of a transitional supersonic jet. Phys Fluids 32(4):046108CrossRef
Zurück zum Zitat Ozawa Y, Saito Y, Nonomura T, Asai K (2021) Aeroacoustic fields of the supersonic twin jets at the ideally expanded condition. to appear in Transactions of the Japan Society for Aeronautical and Space Sciences Ozawa Y, Saito Y, Nonomura T, Asai K (2021) Aeroacoustic fields of the supersonic twin jets at the ideally expanded condition. to appear in Transactions of the Japan Society for Aeronautical and Space Sciences
Zurück zum Zitat Raman G (1999) Supersonic jet screech: half-century from powell to the present. J Sound Vib 225(3):543–571CrossRef Raman G (1999) Supersonic jet screech: half-century from powell to the present. J Sound Vib 225(3):543–571CrossRef
Zurück zum Zitat Sabareesh VB, Srinivasan K, Sundararajan T (2012) Noise characteristics of twin-square slot jets. Int J Aeroacoust 11(5–6):629–650CrossRef Sabareesh VB, Srinivasan K, Sundararajan T (2012) Noise characteristics of twin-square slot jets. Int J Aeroacoust 11(5–6):629–650CrossRef
Zurück zum Zitat Seiner JM, Yu JC (1984) Acoustic near-field properties associated with broadband shock noise. AIAA J 22(9):1207–1215CrossRef Seiner JM, Yu JC (1984) Acoustic near-field properties associated with broadband shock noise. AIAA J 22(9):1207–1215CrossRef
Zurück zum Zitat Seiner JM, Manning JC, Ponton MK (1988) Dynamic pressure loads associated with twin supersonic plume resonance. AIAA J 26(8):954–960CrossRef Seiner JM, Manning JC, Ponton MK (1988) Dynamic pressure loads associated with twin supersonic plume resonance. AIAA J 26(8):954–960CrossRef
Zurück zum Zitat Umeda Y, Ishii R (1997) Oscillation modes of supersonic multijets. J Acoust Soc Am 101(6):3353–3360CrossRef Umeda Y, Ishii R (1997) Oscillation modes of supersonic multijets. J Acoust Soc Am 101(6):3353–3360CrossRef
Zurück zum Zitat Umeda Y, Ishii R (2001) Oscillation modes of supersonic multijets exhausting from very adjacent multiple nozzles. J Acoust Soc Am 110(4):1873–1877CrossRef Umeda Y, Ishii R (2001) Oscillation modes of supersonic multijets exhausting from very adjacent multiple nozzles. J Acoust Soc Am 110(4):1873–1877CrossRef
Zurück zum Zitat Venkatakrishnan L, Wiley A, Kumar R, Alvi F (2011) Density field measurements of a supersonic impinging jet with microjet control. AIAA J 49(2):432–438CrossRef Venkatakrishnan L, Wiley A, Kumar R, Alvi F (2011) Density field measurements of a supersonic impinging jet with microjet control. AIAA J 49(2):432–438CrossRef
Metadaten
Titel
Comparison of three-dimensional density distribution of numerical and experimental analysis for twin jets
verfasst von
Chungil Lee
Yuta Ozawa
Takanori Haga
Taku Nonomura
Keisuke Asai
Publikationsdatum
26.07.2021
Verlag
Springer Berlin Heidelberg
Erschienen in
Journal of Visualization / Ausgabe 6/2021
Print ISSN: 1343-8875
Elektronische ISSN: 1875-8975
DOI
https://doi.org/10.1007/s12650-021-00765-z

Weitere Artikel der Ausgabe 6/2021

Journal of Visualization 6/2021 Zur Ausgabe

Premium Partner