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An experimental investigation of rea...
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University of Michigan.
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An experimental investigation of reacting and nonreacting coaxial jet mixing in a laboratory rocket engine.
紀錄類型:
書目-電子資源 : Monograph/item
正題名/作者:
An experimental investigation of reacting and nonreacting coaxial jet mixing in a laboratory rocket engine./
作者:
Schumaker, Stephen Alexander.
面頁冊數:
219 p.
附註:
Adviser: James F. Driscoll.
Contained By:
Dissertation Abstracts International70-04B.
標題:
Engineering, Aerospace. -
電子資源:
http://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=3354103
ISBN:
9781109113549
An experimental investigation of reacting and nonreacting coaxial jet mixing in a laboratory rocket engine.
Schumaker, Stephen Alexander.
An experimental investigation of reacting and nonreacting coaxial jet mixing in a laboratory rocket engine.
- 219 p.
Adviser: James F. Driscoll.
Thesis (Ph.D.)--University of Michigan, 2009.
Coaxial jets are commonly used as injectors in propulsion and combustion devices due to both the simplicity of their geometry and the rapid mixing they provide. In liquid rocket engines it is common to use coaxial jets in the context of airblast atomization. However, interest exists in developing rocket engines using a full flow staged combustion cycle. In such a configuration both propellants are injected in the gaseous phase. In addition, gaseous coaxial jets have been identified as an ideal test case for the validation of the next generation of injector modeling tools. For these reasons an understanding of the fundamental phenomena which govern mixing in gaseous coaxial jets and the effect of combustion on these phenomena in coaxial jet diffusion flames is needed.
ISBN: 9781109113549Subjects--Topical Terms:
1018395
Engineering, Aerospace.
An experimental investigation of reacting and nonreacting coaxial jet mixing in a laboratory rocket engine.
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Thesis (Ph.D.)--University of Michigan, 2009.
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Coaxial jets are commonly used as injectors in propulsion and combustion devices due to both the simplicity of their geometry and the rapid mixing they provide. In liquid rocket engines it is common to use coaxial jets in the context of airblast atomization. However, interest exists in developing rocket engines using a full flow staged combustion cycle. In such a configuration both propellants are injected in the gaseous phase. In addition, gaseous coaxial jets have been identified as an ideal test case for the validation of the next generation of injector modeling tools. For these reasons an understanding of the fundamental phenomena which govern mixing in gaseous coaxial jets and the effect of combustion on these phenomena in coaxial jet diffusion flames is needed.
520
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A study was performed to better understand the scaling of the stoichiometric mixing length in reacting and nonreacting coaxial jets with velocity ratios greater than one and density ratios less than one. A facility was developed that incorporates a single shear coaxial injector in a laboratory rocket engine capable of ten atmospheres. Optical access allows the use of flame luminosity and laser diagnostic techniques such as Planar Laser Induced Fluorescence (PLIF).
520
$a
Stoichiometric mixing lengths (LS), which are defined as the distance along the centerline where the stoichiometric condition occurs, were measured using PLIF. Acetone was seeded into the center jet to provide direct PLIF measurement of the average and instantaneous mixture fraction fields for a range of momentum flux ratios for the nonreacting cases. For the coaxial jet diffusion flames, LS was measured from OH radical contours. For nonreacting cases the use of a nondimensional momentum flux ratio was found to collapse the mixing length data. The flame lengths of coaxial jet diffusion flames were also found to scale with the momentum flux ratio but different scaling constants are required which depended on the chemistry of the reaction. The effective density ratio was measured which allowed the flame lengths to be collapsed to the nonreacting scaling relation. The equivalence principle of Tacina and Dahm was utilized to compare the theoretical and measured effective density ratios.
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http://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=3354103
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