Particle image velocimetry studies on shock wave diffraction with freestream flow

N. Gongora-Orozco; H. Zare-Behtash; K. Kontis

Particle image velocimetry studies on shock wave diffraction with freestream flow

N. Gongora-Orozco, H. Zare-Behtash, K. Kontis

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

Abstract

The current study presents the effects of a diffracted shock wave interacting with a parallel freestream. The experiments were carried out with diaphragm pressure ratio of P4/P1 = 12, where P 4 and P1 are the driver and driven pressures of the shock tube. Air was used as both the driver and test gas. Freestream velocities of Ufs = 120, 140 and 180 m/s were examined. Particle Image Velocimetry (PIV) was used to quantify the velocity and vorticity fields due to the interaction of unsteady and steady flows. Visualization of the flow features was carried out using the high-speed schlieren photography. The pressure reduction with the highest freestream flow was of 8%, due to the attenuation of the shock/vortex interactions was recorded. Copyright © 2010 by N. Gongora-Orozco, H. Zare-Behtash and K.Kontis.

Original language	English
Title of host publication	48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition\|AIAA Aerosp. Sci. Meet. Incl. New Horiz. Forum Aerosp. Expos.
Publication status	Published - 2010
Event	48th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition - Orlando, FL, United States Duration: 4 Jan 2010 → 7 Jan 2010

Conference

Conference	48th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition
Country/Territory	United States
City	Orlando, FL
Period	4/01/10 → 7/01/10

Keywords

AIAA 2010-876

Cite this

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title = "Particle image velocimetry studies on shock wave diffraction with freestream flow",

abstract = "The current study presents the effects of a diffracted shock wave interacting with a parallel freestream. The experiments were carried out with diaphragm pressure ratio of P4/P1 = 12, where P 4 and P1 are the driver and driven pressures of the shock tube. Air was used as both the driver and test gas. Freestream velocities of Ufs = 120, 140 and 180 m/s were examined. Particle Image Velocimetry (PIV) was used to quantify the velocity and vorticity fields due to the interaction of unsteady and steady flows. Visualization of the flow features was carried out using the high-speed schlieren photography. The pressure reduction with the highest freestream flow was of 8%, due to the attenuation of the shock/vortex interactions was recorded. Copyright {\textcopyright} 2010 by N. Gongora-Orozco, H. Zare-Behtash and K.Kontis.",

keywords = "AIAA 2010-876",

author = "N. Gongora-Orozco and H. Zare-Behtash and K. Kontis",

year = "2010",

language = "English",

isbn = "9781600867392",

booktitle = "48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition|AIAA Aerosp. Sci. Meet. Incl. New Horiz. Forum Aerosp. Expos.",

note = "48th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition ; Conference date: 04-01-2010 Through 07-01-2010",

}

Gongora-Orozco, N, Zare-Behtash, H & Kontis, K 2010, Particle image velocimetry studies on shock wave diffraction with freestream flow. in 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition|AIAA Aerosp. Sci. Meet. Incl. New Horiz. Forum Aerosp. Expos.. 48th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition, Orlando, FL, Florida, United States, 4/01/10.

Particle image velocimetry studies on shock wave diffraction with freestream flow. / Gongora-Orozco, N.; Zare-Behtash, H.; Kontis, K.
48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition|AIAA Aerosp. Sci. Meet. Incl. New Horiz. Forum Aerosp. Expos.. 2010.

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

TY - GEN

T1 - Particle image velocimetry studies on shock wave diffraction with freestream flow

AU - Gongora-Orozco, N.

AU - Zare-Behtash, H.

AU - Kontis, K.

PY - 2010

Y1 - 2010

N2 - The current study presents the effects of a diffracted shock wave interacting with a parallel freestream. The experiments were carried out with diaphragm pressure ratio of P4/P1 = 12, where P 4 and P1 are the driver and driven pressures of the shock tube. Air was used as both the driver and test gas. Freestream velocities of Ufs = 120, 140 and 180 m/s were examined. Particle Image Velocimetry (PIV) was used to quantify the velocity and vorticity fields due to the interaction of unsteady and steady flows. Visualization of the flow features was carried out using the high-speed schlieren photography. The pressure reduction with the highest freestream flow was of 8%, due to the attenuation of the shock/vortex interactions was recorded. Copyright © 2010 by N. Gongora-Orozco, H. Zare-Behtash and K.Kontis.

AB - The current study presents the effects of a diffracted shock wave interacting with a parallel freestream. The experiments were carried out with diaphragm pressure ratio of P4/P1 = 12, where P 4 and P1 are the driver and driven pressures of the shock tube. Air was used as both the driver and test gas. Freestream velocities of Ufs = 120, 140 and 180 m/s were examined. Particle Image Velocimetry (PIV) was used to quantify the velocity and vorticity fields due to the interaction of unsteady and steady flows. Visualization of the flow features was carried out using the high-speed schlieren photography. The pressure reduction with the highest freestream flow was of 8%, due to the attenuation of the shock/vortex interactions was recorded. Copyright © 2010 by N. Gongora-Orozco, H. Zare-Behtash and K.Kontis.

KW - AIAA 2010-876

M3 - Conference contribution

SN - 9781600867392

BT - 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition|AIAA Aerosp. Sci. Meet. Incl. New Horiz. Forum Aerosp. Expos.

T2 - 48th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition

Y2 - 4 January 2010 through 7 January 2010

ER -

Particle image velocimetry studies on shock wave diffraction with freestream flow

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Keywords

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