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CFD Analysis of Fuel Injector Perfor...
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Nelson, Derek .
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CFD Analysis of Fuel Injector Performance Within a Dual Mode Ramjet Combustor.
紀錄類型:
書目-電子資源 : Monograph/item
正題名/作者:
CFD Analysis of Fuel Injector Performance Within a Dual Mode Ramjet Combustor./
作者:
Nelson, Derek .
出版者:
Ann Arbor : ProQuest Dissertations & Theses, : 2020,
面頁冊數:
55 p.
附註:
Source: Masters Abstracts International, Volume: 81-10.
Contained By:
Masters Abstracts International81-10.
標題:
Mechanical engineering. -
電子資源:
https://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=27735508
ISBN:
9781658443852
CFD Analysis of Fuel Injector Performance Within a Dual Mode Ramjet Combustor.
Nelson, Derek .
CFD Analysis of Fuel Injector Performance Within a Dual Mode Ramjet Combustor.
- Ann Arbor : ProQuest Dissertations & Theses, 2020 - 55 p.
Source: Masters Abstracts International, Volume: 81-10.
Thesis (M.S.)--California State University, Long Beach, 2020.
This item must not be sold to any third party vendors.
A dual-mode ramjet concept by NASA researchers Charles J. Trefny and Vance F. Dippold III was expanded upon by analyzing different fuel injector arrangements within the dual mode ramjet's isolator section. Computational fluid dynamics (CFD) analyses were run using Star-CCM+ with varying fuel injector arrangements to see which arrangements would provide the best performance. A 3 step ethylene - oxygen reaction model provided by R. A. Baurle, T. Mathur, M. R. Gruber, and K. R. Jackson was used to model combustion processes. Total pressure, total temperature, and mass fraction plots were used to evaluate the results of CFD analyses.Convergence of the models was met between 24,000 iterations and 45,000 iterations for the three simulations. While there were not large differences in performance between the three simulations, the two injector arrangements performed better, with the staggered fuel injector arrangement having a more valid solution than that of the default fuel injector configuration.
ISBN: 9781658443852Subjects--Topical Terms:
649730
Mechanical engineering.
Subjects--Index Terms:
Computational fluid dynamics
CFD Analysis of Fuel Injector Performance Within a Dual Mode Ramjet Combustor.
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A dual-mode ramjet concept by NASA researchers Charles J. Trefny and Vance F. Dippold III was expanded upon by analyzing different fuel injector arrangements within the dual mode ramjet's isolator section. Computational fluid dynamics (CFD) analyses were run using Star-CCM+ with varying fuel injector arrangements to see which arrangements would provide the best performance. A 3 step ethylene - oxygen reaction model provided by R. A. Baurle, T. Mathur, M. R. Gruber, and K. R. Jackson was used to model combustion processes. Total pressure, total temperature, and mass fraction plots were used to evaluate the results of CFD analyses.Convergence of the models was met between 24,000 iterations and 45,000 iterations for the three simulations. While there were not large differences in performance between the three simulations, the two injector arrangements performed better, with the staggered fuel injector arrangement having a more valid solution than that of the default fuel injector configuration.
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