bookCambridge University Press eBooksSep 12, 2011Closed access

Shock Wave-Boundary-Layer Interactions

University of Cambridge

Indexed incrossref

Abstract

Shock wave-boundary-layer interaction (SBLI) is a fundamental phenomenon in gas dynamics that is observed in many practical situations, ranging from transonic aircraft wings to hypersonic vehicles and engines. SBLIs have the potential to pose serious problems in a flowfield; hence they often prove to be a critical - or even design limiting - issue for many aerospace applications. This is the first book devoted solely to a comprehensive, state-of-the-art explanation of this phenomenon. It includes a description of the basic fluid mechanics of SBLIs plus contributions from leading international experts who share their insight into their physics and the impact they have in practical flow situations. This book is…

Citation impact

749
total citations
FWCI
3.86
Percentile
100%
References
0
Citations per year

Authors

12

Topics & keywords

Keywords
  • Aerodynamics
  • Hypersonic speed
  • Transonic
  • Shock wave
  • Aerospace engineering
  • Shock (circulatory)
  • Boundary layer
  • Phenomenon
No related works found for this paper.