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Numerical Simulation of Lateral Jet in a Supersonic Missile Using Computational Fluid Dynamics
Date
2018-07-03
Author
Dağlı, Efe Can
Aksel, Mehmet Haluk
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https://hdl.handle.net/11511/76526
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In this thesis, numerical simulation method for modelling lateral jet in supersonic crossflow is presented. Lateral jet control provides high maneuverability to the missile at difficult flow conditions. Besides, jet in a crossflow case has a highly complicated flow domain which should be examined using numerical or experimental methods. In this study, numerical methods are used. The thesis consists of two main sections. In the first section, a validation study is conducted for numerical simulation method us...
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E. C. Dağlı and M. H. Aksel, “Numerical Simulation of Lateral Jet in a Supersonic Missile Using Computational Fluid Dynamics,” 2018, Accessed: 00, 2021. [Online]. Available: https://hdl.handle.net/11511/76526.