Shear coaxial injector spray characterization near the LOX post tip region

M. Glogowski; Michael Matthew Micci

Shear coaxial injector spray characterization near the LOX post tip region

M. Glogowski, Michael Matthew Micci

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

Abstract

A characterization of the droplet spray field was performed immediately downstream of the LOX post of a shear coaxial injector using a phase Doppler interferometric device. The tests examined the variation in drop size and mean axial velocity for several post configurations and flow combinations. Injector configurations included recessed or nonrecessed LOX posts having straight or tapered tips. Water and air under atmospheric conditions were used as substitutes to liquid oxygen and gaseous hydrogen. These tests were intended to provide initial insight into the structure of the spray field within a region considered critical to flame stabilization in reacting liquid oxygen and gaseous hydrogen rocket engines.

Original language	English (US)
Title of host publication	31st Joint Propulsion Conference and Exhibit
Publisher	American Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)	9780000000002
State	Published - Jan 1 1995
Event	31st Joint Propulsion Conference and Exhibit, 1995 - San Diego, United States Duration: Jul 10 1995 → Jul 12 1995

Publication series

Name	31st Joint Propulsion Conference and Exhibit

Other

Other	31st Joint Propulsion Conference and Exhibit, 1995
Country/Territory	United States
City	San Diego
Period	7/10/95 → 7/12/95

All Science Journal Classification (ASJC) codes

Energy Engineering and Power Technology
Electrical and Electronic Engineering
Mechanical Engineering
Control and Systems Engineering
Aerospace Engineering

Cite this

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title = "Shear coaxial injector spray characterization near the LOX post tip region",

abstract = "A characterization of the droplet spray field was performed immediately downstream of the LOX post of a shear coaxial injector using a phase Doppler interferometric device. The tests examined the variation in drop size and mean axial velocity for several post configurations and flow combinations. Injector configurations included recessed or nonrecessed LOX posts having straight or tapered tips. Water and air under atmospheric conditions were used as substitutes to liquid oxygen and gaseous hydrogen. These tests were intended to provide initial insight into the structure of the spray field within a region considered critical to flame stabilization in reacting liquid oxygen and gaseous hydrogen rocket engines.",

author = "M. Glogowski and Micci, {Michael Matthew}",

year = "1995",

month = jan,

day = "1",

language = "English (US)",

isbn = "9780000000002",

series = "31st Joint Propulsion Conference and Exhibit",

publisher = "American Institute of Aeronautics and Astronautics Inc, AIAA",

booktitle = "31st Joint Propulsion Conference and Exhibit",

note = "31st Joint Propulsion Conference and Exhibit, 1995 ; Conference date: 10-07-1995 Through 12-07-1995",

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Shear coaxial injector spray characterization near the LOX post tip region. / Glogowski, M.; Micci, Michael Matthew.
31st Joint Propulsion Conference and Exhibit. American Institute of Aeronautics and Astronautics Inc, AIAA, 1995. AIAA 95-2552 (31st Joint Propulsion Conference and Exhibit).

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

TY - GEN

T1 - Shear coaxial injector spray characterization near the LOX post tip region

AU - Glogowski, M.

AU - Micci, Michael Matthew

PY - 1995/1/1

Y1 - 1995/1/1

N2 - A characterization of the droplet spray field was performed immediately downstream of the LOX post of a shear coaxial injector using a phase Doppler interferometric device. The tests examined the variation in drop size and mean axial velocity for several post configurations and flow combinations. Injector configurations included recessed or nonrecessed LOX posts having straight or tapered tips. Water and air under atmospheric conditions were used as substitutes to liquid oxygen and gaseous hydrogen. These tests were intended to provide initial insight into the structure of the spray field within a region considered critical to flame stabilization in reacting liquid oxygen and gaseous hydrogen rocket engines.

AB - A characterization of the droplet spray field was performed immediately downstream of the LOX post of a shear coaxial injector using a phase Doppler interferometric device. The tests examined the variation in drop size and mean axial velocity for several post configurations and flow combinations. Injector configurations included recessed or nonrecessed LOX posts having straight or tapered tips. Water and air under atmospheric conditions were used as substitutes to liquid oxygen and gaseous hydrogen. These tests were intended to provide initial insight into the structure of the spray field within a region considered critical to flame stabilization in reacting liquid oxygen and gaseous hydrogen rocket engines.

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M3 - Conference contribution

AN - SCOPUS:84964490229

SN - 9780000000002

T3 - 31st Joint Propulsion Conference and Exhibit

BT - 31st Joint Propulsion Conference and Exhibit

PB - American Institute of Aeronautics and Astronautics Inc, AIAA

T2 - 31st Joint Propulsion Conference and Exhibit, 1995

Y2 - 10 July 1995 through 12 July 1995

ER -

Shear coaxial injector spray characterization near the LOX post tip region

Abstract

Publication series

Other

All Science Journal Classification (ASJC) codes

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