Numerical investigation of the effects of wall heating and cooling on the nonlinear transition stages for a sharp cone at Mach 6-Reference-Cited by-同舟云学术

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Numerical investigation of the effects of wall heating and cooling on the nonlinear transition stages for a sharp cone at Mach 6

Published:2022-01-03 Issue: Volume: Page:
ISSN:
Container-title:AIAA SCITECH 2022 Forum
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Author:

Herman Briannah¹,Hader Christoph¹,Fasel Hermann F.¹

Affiliation:

1. The University of Arizona

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2022-0601

Reference44 articles.

1. Chynoweth, B. “Measurements of transition dominated by the second-mode instability at Mach 6,” Ph.D. thesis,Purdue University, 2018.

2. Laible, A. C. “Numerical Investigation of Boundary Layer Transition for cones at Mach 3.5 and 6.0,” Ph.D. thesis,The University of Arizona, 2011.

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1. Numerical investigation of the nonlinear transition stages for a sharp cone at Mach 10;AIAA AVIATION 2022 Forum;2022-06-20

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