Combined Magnetohydrodynamic and Geometric Optimization of a Hypersonic Inlet

This paper considers the numerical optimization of a double ramp scramjet inlet using magnetohydrodynamic (MHD) effects together with inlet ramp angle changes. The parameter being optimized is the mass cap...

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Main Authors: Kamesh Subbarao, Jennifer D. Goss
Format: Article
Language:English
Published: Wiley 2009-01-01
Series:International Journal of Aerospace Engineering
Online Access:http://dx.doi.org/10.1155/2009/793647
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author Kamesh Subbarao
Jennifer D. Goss
author_facet Kamesh Subbarao
Jennifer D. Goss
author_sort Kamesh Subbarao
collection DOAJ
description This paper considers the numerical optimization of a double ramp scramjet inlet using magnetohydrodynamic (MHD) effects together with inlet ramp angle changes. The parameter being optimized is the mass capture at the throat of the inlet, such that spillage effects for less than design Mach numbers are reduced. The control parameters for the optimization include the MHD effects in conjunction with ramp angle changes. To enhance the MHD effects different ionization scenarios depending upon the alignment of the magnetic field are considered. The flow solution is based on the Advection Upstream Splitting Method (AUSM) that accounts for the MHD source terms as well. A numerical Broyden-Flecher-Goldfarb-Shanno- (BFGS-) based procedure is utilized to optimize the inlet mass capture. Numerical validation results compared to published results in the literature as well as the outcome of the optimization procedure are summarized to illustrate the efficacy of the approach.
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institution Kabale University
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language English
publishDate 2009-01-01
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record_format Article
series International Journal of Aerospace Engineering
spelling doaj-art-e15a0d62c4cb40ea957eb7b75065922b2025-02-03T05:54:11ZengWileyInternational Journal of Aerospace Engineering1687-59661687-59742009-01-01200910.1155/2009/793647793647Combined Magnetohydrodynamic and Geometric Optimization of a Hypersonic InletKamesh Subbarao0Jennifer D. Goss1Department of Mechanical and Aerospace Engineering, The University of Texas, Arlington, TX 76019, USADepartment of Mechanical and Aerospace Engineering, The University of Texas, Arlington, TX 76019, USAThis paper considers the numerical optimization of a double ramp scramjet inlet using magnetohydrodynamic (MHD) effects together with inlet ramp angle changes. The parameter being optimized is the mass capture at the throat of the inlet, such that spillage effects for less than design Mach numbers are reduced. The control parameters for the optimization include the MHD effects in conjunction with ramp angle changes. To enhance the MHD effects different ionization scenarios depending upon the alignment of the magnetic field are considered. The flow solution is based on the Advection Upstream Splitting Method (AUSM) that accounts for the MHD source terms as well. A numerical Broyden-Flecher-Goldfarb-Shanno- (BFGS-) based procedure is utilized to optimize the inlet mass capture. Numerical validation results compared to published results in the literature as well as the outcome of the optimization procedure are summarized to illustrate the efficacy of the approach.http://dx.doi.org/10.1155/2009/793647
spellingShingle Kamesh Subbarao
Jennifer D. Goss
Combined Magnetohydrodynamic and Geometric Optimization of a Hypersonic Inlet
International Journal of Aerospace Engineering
title Combined Magnetohydrodynamic and Geometric Optimization of a Hypersonic Inlet
title_full Combined Magnetohydrodynamic and Geometric Optimization of a Hypersonic Inlet
title_fullStr Combined Magnetohydrodynamic and Geometric Optimization of a Hypersonic Inlet
title_full_unstemmed Combined Magnetohydrodynamic and Geometric Optimization of a Hypersonic Inlet
title_short Combined Magnetohydrodynamic and Geometric Optimization of a Hypersonic Inlet
title_sort combined magnetohydrodynamic and geometric optimization of a hypersonic inlet
url http://dx.doi.org/10.1155/2009/793647
work_keys_str_mv AT kameshsubbarao combinedmagnetohydrodynamicandgeometricoptimizationofahypersonicinlet
AT jenniferdgoss combinedmagnetohydrodynamicandgeometricoptimizationofahypersonicinlet