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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Citation Formats

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.