Skip to main content

2018 | OriginalPaper | Buchkapitel

Experimental Studies on the Receptivity of Stationary Crossflow Modes to Pneumatic Actuation

verfasst von : J. Lohse, A. Berthold, W. Nitsche

Erschienen in: New Results in Numerical and Experimental Fluid Mechanics XI

Verlag: Springer International Publishing

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

search-config
loading …

Abstract

The influence of spanwise periodic steady blowing or suction on the development of stationary crossflow vortices is investigated experimentally in a three-dimensional boundary-layer flow. Different jet-outlet geometries were tested to control the naturally most amplified crossflow mode in this scenario. Although bypass transition at the actuator orifices is an issue in the blowing cases, the strongest receptivity was observed for steady blowing against the direction of the crossflow veloctiy component.

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 "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!

Literatur
1.
Zurück zum Zitat Bippes, H.: Basic experiments on transition in three-dimensional boundary layers dominated by crossflow instability. Prog. Aerosp. Sci. 35(4), 363–412 (1999)CrossRef Bippes, H.: Basic experiments on transition in three-dimensional boundary layers dominated by crossflow instability. Prog. Aerosp. Sci. 35(4), 363–412 (1999)CrossRef
2.
Zurück zum Zitat Carpenter, A., Saric, W., Reed, H.: Laminar flow control on a swept wing with distributed roughness. AIAA Paper 2008–7335, 1–9 (2008) Carpenter, A., Saric, W., Reed, H.: Laminar flow control on a swept wing with distributed roughness. AIAA Paper 2008–7335, 1–9 (2008)
3.
Zurück zum Zitat Hosseini, S., Tempelmann, D., Hanifi, A., Henningson, D.: Stabilization of a swept-wing boundary layer by distributed roughness elements. J. Fluid Mech. 718 (2013) Hosseini, S., Tempelmann, D., Hanifi, A., Henningson, D.: Stabilization of a swept-wing boundary layer by distributed roughness elements. J. Fluid Mech. 718 (2013)
4.
Zurück zum Zitat Lohse, J., Barth, H., Nitsche, W.: Active control of crossflow-induced transition by means of in-line pneumatic actuator orifices. Exp. Fluids 57(8), 1–10 (2016)CrossRef Lohse, J., Barth, H., Nitsche, W.: Active control of crossflow-induced transition by means of in-line pneumatic actuator orifices. Exp. Fluids 57(8), 1–10 (2016)CrossRef
5.
Zurück zum Zitat Messing, R., Kloker, M.: Investigation of suction for laminar flow control of three-dimensional boundary layers. J. Fluid Mech. 658, 117–147 (2010)CrossRefMATH Messing, R., Kloker, M.: Investigation of suction for laminar flow control of three-dimensional boundary layers. J. Fluid Mech. 658, 117–147 (2010)CrossRefMATH
6.
Zurück zum Zitat Saric, W., Carrillo, R., Reibert, M.: Leading-edge roughness as a transition control mechanism. AIAA Paper 98–0781, 1–13 (1998) Saric, W., Carrillo, R., Reibert, M.: Leading-edge roughness as a transition control mechanism. AIAA Paper 98–0781, 1–13 (1998)
7.
Zurück zum Zitat Saric, W., Reed, H.L., White, E.: Stability and transition of three-dimensional boundary layers. Annu. Rev. Fluid Mech. 35, 413–439 (2003)CrossRefMATHMathSciNet Saric, W., Reed, H.L., White, E.: Stability and transition of three-dimensional boundary layers. Annu. Rev. Fluid Mech. 35, 413–439 (2003)CrossRefMATHMathSciNet
9.
Zurück zum Zitat Serpieri, J., Kotsonis, M.: Three-dimensional organisation of primary and secondary crossflow instability. J. Fluid Mech. 799, 200–245 (2016)CrossRef Serpieri, J., Kotsonis, M.: Three-dimensional organisation of primary and secondary crossflow instability. J. Fluid Mech. 799, 200–245 (2016)CrossRef
10.
Zurück zum Zitat Treaster, Y.: The calibration and application of five-hole probes. ISA Trans. 18(3) (1979) Treaster, Y.: The calibration and application of five-hole probes. ISA Trans. 18(3) (1979)
11.
Zurück zum Zitat Wassermann, P., Kloker, M.: Mechanisms and passive control of crossflow-vortex-induced transition in a three-dimensional boundary layer. J. Fluid Mech. 456, 49–84 (2002)CrossRefMATHMathSciNet Wassermann, P., Kloker, M.: Mechanisms and passive control of crossflow-vortex-induced transition in a three-dimensional boundary layer. J. Fluid Mech. 456, 49–84 (2002)CrossRefMATHMathSciNet
12.
Zurück zum Zitat White, E., Saric, W.S.: Application of variable leading-edge roughness for transition control on swept wings. AIAA Conf. Proc. Paper 2000–0283, 1–11 (2000) White, E., Saric, W.S.: Application of variable leading-edge roughness for transition control on swept wings. AIAA Conf. Proc. Paper 2000–0283, 1–11 (2000)
Metadaten
Titel
Experimental Studies on the Receptivity of Stationary Crossflow Modes to Pneumatic Actuation
verfasst von
J. Lohse
A. Berthold
W. Nitsche
Copyright-Jahr
2018
DOI
https://doi.org/10.1007/978-3-319-64519-3_24

    Marktübersichten

    Die im Laufe eines Jahres in der „adhäsion“ veröffentlichten Marktübersichten helfen Anwendern verschiedenster Branchen, sich einen gezielten Überblick über Lieferantenangebote zu verschaffen.