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Design optimization in chemically reacting flows
Date
2011-12-01
Author
Yumuşak, M.
Eyi, Sinan
Metadata
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The objective of this study is to develop a reliable and efficient design tool that can be used in chemically reacting flows. The flow analysis is based on axisymmetric Euler and the finite rate chemical reaction equations. These coupled equations are solved by using Newton's method. Both numerical and analytical methods are used to calculate Jacobian matrices. Sensitivities are evaluated by using adjoint method. The performance of the optimization method is demonstrated for a rocket motor nozzle design. © 2011 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.
Subject Keywords
Essentially non-oscillatory schemes
,
WENO Scheme
,
Hyperbolic conservation laws
URI
https://www.scopus.com/inward/record.uri?partnerID=HzOxMe3b&scp=84880617987&origin=inward
https://hdl.handle.net/11511/74016
Conference Name
20th AIAA Computational Fluid Dynamics Conference 2011
Collections
Department of Aerospace Engineering, Conference / Seminar
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M. Yumuşak and S. Eyi, “Design optimization in chemically reacting flows,” Honolulu, HI, Amerika Birleşik Devletleri, 2011, Accessed: 00, 2021. [Online]. Available: https://www.scopus.com/inward/record.uri?partnerID=HzOxMe3b&scp=84880617987&origin=inward.