Localized flow control by laser energy deposition applied to Edney IV shock impingement and intersecting shocks

Russell G. Adelgren; Hong Yan; Gregory S. Elliott; Doyle D. Knight; Thomas J. Beutner; Alexander A. Zheltovodov; Mikhail Ivanod; Dmitri Khotyanovsky

Localized flow control by laser energy deposition applied to Edney IV shock impingement and intersecting shocks

Russell G. Adelgren, Hong Yan, Gregory S. Elliott, Doyle D. Knight, Thomas J. Beutner, Alexander A. Zheltovodov, Mikhail Ivanod, Dmitri Khotyanovsky

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

Abstract

Laser induced optical breakdown has been demonstrated as a method for local modification of the shock structure in supersonic flows. Two specific applications at Mach 3.45 are considered: an Edney IV interaction and the intersection of symmetric shock waves in the dual solution domain. Experiments were performed for both cases with detailed flow visualization and quantitatke measurements. Numerical simulations were performed for the crossing shock case and demonstrated the capability for a Mach Reflection to Regular Reflection transition and the Regular Reflection to Mach Reflection transition in the Dual Solution Domain.

Original language	English (US)
Title of host publication	41st Aerospace Sciences Meeting and Exhibit
State	Published - 2003
Externally published	Yes
Event	41st Aerospace Sciences Meeting and Exhibit 2003 - Reno, NV, United States Duration: Jan 6 2003 → Jan 9 2003

Publication series

Name	41st Aerospace Sciences Meeting and Exhibit

Other

Other	41st Aerospace Sciences Meeting and Exhibit 2003
Country/Territory	United States
City	Reno, NV
Period	1/6/03 → 1/9/03

ASJC Scopus subject areas

Space and Planetary Science
Aerospace Engineering

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Adelgren, RG, Yan, H, Elliott, GS, Knight, DD, Beutner, TJ, Zheltovodov, AA, Ivanod, M & Khotyanovsky, D 2003, Localized flow control by laser energy deposition applied to Edney IV shock impingement and intersecting shocks. in 41st Aerospace Sciences Meeting and Exhibit. 41st Aerospace Sciences Meeting and Exhibit, 41st Aerospace Sciences Meeting and Exhibit 2003, Reno, NV, United States, 1/6/03.

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title = "Localized flow control by laser energy deposition applied to Edney IV shock impingement and intersecting shocks",

abstract = "Laser induced optical breakdown has been demonstrated as a method for local modification of the shock structure in supersonic flows. Two specific applications at Mach 3.45 are considered: an Edney IV interaction and the intersection of symmetric shock waves in the dual solution domain. Experiments were performed for both cases with detailed flow visualization and quantitatke measurements. Numerical simulations were performed for the crossing shock case and demonstrated the capability for a Mach Reflection to Regular Reflection transition and the Regular Reflection to Mach Reflection transition in the Dual Solution Domain.",

author = "Adelgren, {Russell G.} and Hong Yan and Elliott, {Gregory S.} and Knight, {Doyle D.} and Beutner, {Thomas J.} and Zheltovodov, {Alexander A.} and Mikhail Ivanod and Dmitri Khotyanovsky",

year = "2003",

language = "English (US)",

isbn = "9781624100994",

series = "41st Aerospace Sciences Meeting and Exhibit",

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note = "41st Aerospace Sciences Meeting and Exhibit 2003 ; Conference date: 06-01-2003 Through 09-01-2003",

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T1 - Localized flow control by laser energy deposition applied to Edney IV shock impingement and intersecting shocks

AU - Adelgren, Russell G.

AU - Yan, Hong

AU - Elliott, Gregory S.

AU - Knight, Doyle D.

AU - Beutner, Thomas J.

AU - Zheltovodov, Alexander A.

AU - Ivanod, Mikhail

AU - Khotyanovsky, Dmitri

PY - 2003

Y1 - 2003

N2 - Laser induced optical breakdown has been demonstrated as a method for local modification of the shock structure in supersonic flows. Two specific applications at Mach 3.45 are considered: an Edney IV interaction and the intersection of symmetric shock waves in the dual solution domain. Experiments were performed for both cases with detailed flow visualization and quantitatke measurements. Numerical simulations were performed for the crossing shock case and demonstrated the capability for a Mach Reflection to Regular Reflection transition and the Regular Reflection to Mach Reflection transition in the Dual Solution Domain.

AB - Laser induced optical breakdown has been demonstrated as a method for local modification of the shock structure in supersonic flows. Two specific applications at Mach 3.45 are considered: an Edney IV interaction and the intersection of symmetric shock waves in the dual solution domain. Experiments were performed for both cases with detailed flow visualization and quantitatke measurements. Numerical simulations were performed for the crossing shock case and demonstrated the capability for a Mach Reflection to Regular Reflection transition and the Regular Reflection to Mach Reflection transition in the Dual Solution Domain.

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M3 - Conference contribution

AN - SCOPUS:79751528528

SN - 9781624100994

T3 - 41st Aerospace Sciences Meeting and Exhibit

BT - 41st Aerospace Sciences Meeting and Exhibit

T2 - 41st Aerospace Sciences Meeting and Exhibit 2003

Y2 - 6 January 2003 through 9 January 2003

ER -

Localized flow control by laser energy deposition applied to Edney IV shock impingement and intersecting shocks

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