Combined Magnetohydrodynamic and Geometric Optimization of a Hypersonic Inlet
Author:
Affiliation:
1. Department of Mechanical and Aerospace Engineering, The University of Texas, Arlington, TX 76019, USA
Abstract
Funder
HyperComp Inc.
Publisher
Hindawi Limited
Subject
Aerospace Engineering
Link
http://downloads.hindawi.com/journals/ijae/2009/793647.pdf
Reference14 articles.
1. Optimization of contoured hypersonic scramjet inlets with a least-squares parabolized Navier-Stokes procedure
2. The optimization of a magnetohydrodynamic generating duct
3. Magnetohydrodynamic Control on Hypersonic Aircraft Under "Ajax" Concept
4. Magnetohydrodynamic and Electrohydrodynamic Control of Hypersonic Flows of Weakly Ionized Plasmas
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