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CFD Analysis of Fuel Injector Perfor...

Nelson, Derek .

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CFD Analysis of Fuel Injector Performance Within a Dual Mode Ramjet Combustor.

Record Type:	Electronic resources : Monograph/item
Title/Author:	CFD Analysis of Fuel Injector Performance Within a Dual Mode Ramjet Combustor./
Author:	Nelson, Derek .
Published:	Ann Arbor : ProQuest Dissertations & Theses, : 2020,
Description:	55 p.
Notes:	Source: Masters Abstracts International, Volume: 81-10.
Contained By:	Masters Abstracts International81-10.
Subject:	Mechanical engineering. -
Online resource:	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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245 1 0 $a CFD Analysis of Fuel Injector Performance Within a Dual Mode Ramjet Combustor.
260 1 $a Ann Arbor : $b ProQuest Dissertations & Theses, $c 2020
300 $a 55 p.
500 $a Source: Masters Abstracts International, Volume: 81-10.
500 $a Advisor: Chen, Hsun-Hu.
502 $a Thesis (M.S.)--California State University, Long Beach, 2020.
506 $a This item must not be sold to any third party vendors.
520 $a 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.
590 $a School code: 6080.
650 4 $a Mechanical engineering. $3 649730
650 4 $a Computational physics. $3 3343998
650 4 $a Aerospace engineering. $3 1002622
653 $a Computational fluid dynamics
653 $a Combustion
653 $a Ramjet
653 $a Scramjet
690 $a 0548
690 $a 0216
690 $a 0538
710 2 $a California State University, Long Beach. $b Mechanical and Aerospace Engineering. $3 3184783
773 0 $t Masters Abstracts International $g 81-10.
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791 $a M.S.
792 $a 2020
793 $a English
856 4 0 $u https://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=27735508