Design optimization of a 2-d scramjet inlet

Date

2019-05-14

Author

Başaran, Mehmet
Leblebici, Engin
Tuncer, İsmail Hakkı

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A generic 2-D scramjet inlet is analyzed with SU2 software. Accuracy of three turbulence models are compared and a mesh dependence study is performed for the case. Results are compared favorably with experimental data from Idris et al. (2014). The geometry is planned to be optimized by using the adjoint method in the full paper.

Subject Keywords

SU2, Scramjet inlets, Design optimization, Adjoint methods, Turbulence models

URI

http://www.parcfd.org/2019/
https://hdl.handle.net/11511/76257

Conference Name

31st International Conference on Parallel Computational Fluid Dynamics, (May 14-17, 2019)

Collections

Department of Aerospace Engineering, Conference / Seminar

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Citation Formats

M. Başaran, E. Leblebici, and İ. H. Tuncer, “Design optimization of a 2-d scramjet inlet ,” presented at the 31st International Conference on Parallel Computational Fluid Dynamics, (May 14-17, 2019), Antalya, Türkiye, 2019, Accessed: 00, 2021. [Online]. Available: http://www.parcfd.org/2019/.