Turbulent diffusion flux of transverse jet into pseudo-shock wave

Taekjin Lee, Toshinori Kouchi, Yoshinori Oka, Goro Masuya

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

An experiment to investigate the effect of pseudo-shock wave (PSW) on turbulent diffusion of a transverse jet in a Mach 2.0 supersonic crossflow was conducted. The vertical jet from a 2.5 mm-diameter orifice was injected into pseudo-shock wave and jetto-crossflow momentum flux ratio was 2.2. To measure turbulent diffusion flux, stereoscopic particle image velocimetry (SPIV) and acetone planar laser-induced fluorescence (PLIF) system were combined and velocity and concentration fields were simultaneously measured. Measurement plane was a cross section at 10 mm downstream from the injection port. The position of PSW was controlled by a flow plug at the duct exit driven by a stepping motor. The front of PSW was set at 30 mm upstream from the orifice. Without PSW, turbulent diffusion flux (TDF) of the injectant was extended upward and the shape of injectant plume was deformed by a counter-rotating vortex pair (CVP) which was formed behind the injected gas. Under PSW, the CVP made horseshoe-shape concentration distribution. TDF directed from spur of concentration to both free stream side and lee side of the jet. Most of no-PSW condition and outward of under-PSW TDF was concentration-fluctuation-dominant, only inward TDF under PSW emerged as turbulent-dominant. The effect of PSW that enhances diffusion of injected gas was confirmed.

Original languageEnglish
Title of host publication54th AIAA Aerospace Sciences Meeting
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)9781624103933
Publication statusPublished - 2016
Event54th AIAA Aerospace Sciences Meeting, 2016 - San Diego, United States
Duration: Jan 4 2016Jan 8 2016

Other

Other54th AIAA Aerospace Sciences Meeting, 2016
CountryUnited States
CitySan Diego
Period1/4/161/8/16

Fingerprint

Shock waves
Fluxes
Orifices
Vortex flow
Stepping motors
Gases
Acetone
Velocity measurement
Ducts
Mach number
Momentum
Fluorescence
Lasers

ASJC Scopus subject areas

  • Aerospace Engineering

Cite this

Lee, T., Kouchi, T., Oka, Y., & Masuya, G. (2016). Turbulent diffusion flux of transverse jet into pseudo-shock wave. In 54th AIAA Aerospace Sciences Meeting American Institute of Aeronautics and Astronautics Inc, AIAA.

Turbulent diffusion flux of transverse jet into pseudo-shock wave. / Lee, Taekjin; Kouchi, Toshinori; Oka, Yoshinori; Masuya, Goro.

54th AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics Inc, AIAA, 2016.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Lee, T, Kouchi, T, Oka, Y & Masuya, G 2016, Turbulent diffusion flux of transverse jet into pseudo-shock wave. in 54th AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics Inc, AIAA, 54th AIAA Aerospace Sciences Meeting, 2016, San Diego, United States, 1/4/16.
Lee T, Kouchi T, Oka Y, Masuya G. Turbulent diffusion flux of transverse jet into pseudo-shock wave. In 54th AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics Inc, AIAA. 2016
Lee, Taekjin ; Kouchi, Toshinori ; Oka, Yoshinori ; Masuya, Goro. / Turbulent diffusion flux of transverse jet into pseudo-shock wave. 54th AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics Inc, AIAA, 2016.
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