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Hypersonic boundary layer transitions over a yawed, blunt cone

  • Published:2021-12 Issue: Volume:119 Page:107170
  • ISSN:1270-9638
  • Container-title:Aerospace Science and Technology
  • language:en
  • Short-container-title:Aerospace Science and Technology

Author:

Chen J.,Dong S.,Chen X.,Xu G.,Yuan X.ORCID

Funder

National Key Research and Development Program of China

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference43 articles.

1. Instability on a hypersonic yawed straight cone;Perez,2013

2. Laminar to turbulent transition on the HIRiRE-1 cone at Mach 7 and high angle of attack;Willems,2014

3. Instability modes in boundary layers of an inclined cone at Mach 6;Muñoz;J. Spacecr. Rockets,2014

4. Crossflow instability in a hypersonic boundary layer;Craig;J. Fluid Mech.,2016

5. Possible secondary instability of stationary crossflow vortices on an inclined cone at Mach 6;Ward,2015
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