A. Obraz , N. Palchekovskaya , I. Egorov , A. Fedorov

DOI Number XXX-YYY-ZZZ (DOI probably already generated by Elsevier)

Conference Number HiSST 2018_31501116

The effect of wall normal gas injection on the boundary layer stability is simulated numerically for the hypersonic flow over the blunted body at Mach number 7.32. The boundary layer stability is analyzed with the linear stability theory and e-N method. For all cases considered, the critical N-factors at the experimentally observed loci of the transition onset do not exceed 1.5. This indicates the bypass scenario of the laminar-turbulent transition. The correlation is observed between the computed critical stability points and experimental transition onset loci at various intensities of the injection

Read the full paper from the Elsevier website >

In Categories: Boundary Layer Control, HiSST 2018, Materials and Structures, Propulsion Systems and Components
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.