articleProgress in Aerospace SciencesNov 17, 2014Closed access

Progress in shock wave/boundary layer interactions

The Ohio State University

Indexed incrossref

Abstract

No abstract available for this paper.

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649
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FWCI
21.24
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100%
References
178
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Authors

1

Topics & keywords

Keywords
  • Boundary layer
  • Scramjet
  • Aerospace engineering
  • Hypersonic speed
  • Flow separation
  • Mechanics
  • Heat transfer
  • Laminar flow
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