Detailed measurements on unsteady properties in three-dimensional shock wave/turbulent boundary layer interaction induced by blunt fin at Mach number 4

Shigeru Aso, Seishi Kuranaga, Masanori Hayashi

Research output: Contribution to conferencePaper

4 Citations (Scopus)

Abstract

Turbulent properties in the shock wave/turbulent boundary layer interaction induced by blunt fins with semi-cylindrical leading edge have been investigated. Flow fields are visualized by the Schlieren method and the oil flow technique. Pressure fluctuations are measured in the whole interaction region in order to understand the phenomena and provide sufficient information for turbulent modeling. Distributions of standard deviations and higher moments of pressure fluctuations are also measured. Quite complicated distributions of standard deviations and higher moments of pressure fluctuations are obtained. Those properties show significant changes in the interaction region and quite interesting characteristics are observed. Also in tire interaction region intermittent phenomena due to the shock wave motion are observed. Those complicated results suggest that more sophisticated turbulent modeling is necessary to simulate the flow field.

Original languageEnglish
Publication statusPublished - Jan 1 1991
EventAIAA 22nd Fluid Dynamics, Plasma Dynamics and Lasers Conference, 1991 - Honolulu, United States
Duration: Jun 24 1991Jun 26 1991

Other

OtherAIAA 22nd Fluid Dynamics, Plasma Dynamics and Lasers Conference, 1991
CountryUnited States
CityHonolulu
Period6/24/916/26/91

Fingerprint

turbulent boundary layer
fins
Mach number
Shock waves
shock waves
Boundary layers
Flow fields
standard deviation
flow distribution
interactions
moments
Tires
tires
leading edges
oils

All Science Journal Classification (ASJC) codes

  • Engineering (miscellaneous)
  • Aerospace Engineering
  • Electrical and Electronic Engineering
  • Condensed Matter Physics

Cite this

Aso, S., Kuranaga, S., & Hayashi, M. (1991). Detailed measurements on unsteady properties in three-dimensional shock wave/turbulent boundary layer interaction induced by blunt fin at Mach number 4. Paper presented at AIAA 22nd Fluid Dynamics, Plasma Dynamics and Lasers Conference, 1991, Honolulu, United States.

Detailed measurements on unsteady properties in three-dimensional shock wave/turbulent boundary layer interaction induced by blunt fin at Mach number 4. / Aso, Shigeru; Kuranaga, Seishi; Hayashi, Masanori.

1991. Paper presented at AIAA 22nd Fluid Dynamics, Plasma Dynamics and Lasers Conference, 1991, Honolulu, United States.

Research output: Contribution to conferencePaper

Aso, S, Kuranaga, S & Hayashi, M 1991, 'Detailed measurements on unsteady properties in three-dimensional shock wave/turbulent boundary layer interaction induced by blunt fin at Mach number 4', Paper presented at AIAA 22nd Fluid Dynamics, Plasma Dynamics and Lasers Conference, 1991, Honolulu, United States, 6/24/91 - 6/26/91.
Aso S, Kuranaga S, Hayashi M. Detailed measurements on unsteady properties in three-dimensional shock wave/turbulent boundary layer interaction induced by blunt fin at Mach number 4. 1991. Paper presented at AIAA 22nd Fluid Dynamics, Plasma Dynamics and Lasers Conference, 1991, Honolulu, United States.
Aso, Shigeru ; Kuranaga, Seishi ; Hayashi, Masanori. / Detailed measurements on unsteady properties in three-dimensional shock wave/turbulent boundary layer interaction induced by blunt fin at Mach number 4. Paper presented at AIAA 22nd Fluid Dynamics, Plasma Dynamics and Lasers Conference, 1991, Honolulu, United States.
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