Jeroen Van den Eynde & Johan Steelant

DOI Number XXX-YYY-ZZZ

Conference Number HiSST 2018-1300826

A two-equation correlation-based transition model is presented to predict the onset and development of the laminar-turbulent transition process for boundary layers. It uses one equation for the intermittencytransport, and another for the transport of a transition onset criterion. It uses some elements from the Langtry-Menter intermittency-based γ-Reθt transition model, but introduces a physics-based rationale for the intermittency production and destruction. The model has been validated for a number of subsonic to hypersonic boundary layer cases and is able to correctly predict the transition onset location and typical skin friction overshoot.

Download the Full Paper >

Email
Print
LinkedIn
The paper above was part of  proceedings of a CEAS event and as such the author has signed a publication agreement to have their paper published in the repository. In the case this paper is found somewhere else CEAS always links to the other source.  CEAS takes great care in making the correct content available to the reader. If any mistakes are found  in the listings please contact us directly at papers@aerospacerepository.org and we will correct the listing promptly.  CEAS cannot be held liable either for mistakes in editorial or technical aspects, nor for omissions, nor for the correctness of the content. In particular, CEAS does not guarantee completeness or correctness of information contained in external websites which can be accessed via links from CEAS’s websites. Despite accurate research on the content of such linked external websites, CEAS cannot be held liable for their content. Only the content providers of such external sites are liable for their content. Should you notice any mistake in technical or editorial aspects of the CEAS site, please do not hesitate to inform us.